
 p r o g r a m  C A I S S O N _ V H M  w32 version 00.12_b04 
 ------------------------------------  at 16:56:44 on 19-AUG-2024
 caisson foundation resistance in undrained soil during VHM load.
 (c) S.Kay Consultant, Leiderdorp, The Netherlands.
 Please read the CAISSON_VHM Users Manual [ref SKA/MAN/003]
         and the CAISSON_VHM FAQ File     [ref SKA/FAQ/003].


 datain_caisson: < --- BEGIN

 pidata: < --- BEGIN
 pidata: input  text file: "JOB.I01"
       : output text file: "JOB.O01"
       : output plot file: "D4.5_PEN15_ZLUG9_SLIDING.O1B.PDF"
       : program name    : "CAISSON_VHM"

 pidata: rtitle          : "RUN 1B: AS RUN 1 BUT NLC=10 (WAS 1) AND T_LUG = 0 THRU 90DEG"
       : ptitle          : "EXAMPLE MODE22"
       : projno          : "SKA/MAN/003"
       : locatn          : "CAISSON_VHM"

 pidata: END --- >


 gmdata: < --- BEGIN
 numsl
    4
  zdep        bden       su_top      su_bot   
   [m]     [kN/m^3]      [kPa]        [kPa]   
    0.00        4.00        1.00        4.00    
   0.700        4.00        4.00        6.50    
    4.60        5.00        6.50        19.0    
    18.0        5.00        19.0        41.0    
    40.0    
 m_fac
    1.30    
 gmdata: END --- >


 psdata: < --- BEGIN
 psdata: vhm_model
 KAY+PALIX_2011
 MODE_VHM
   22
 psdata: END --- >


 cfdata: < --- BEGIN
 ncgeom
    5
 cgeom
 CIRCULAR
 nfhxp  wt_D_side  wt_D_top
  0   0.780E-02   0.111E-01
 iro_lug  r_lug_user
  1    0.00    
 D  L  zlug
   4.50  15.00  10.00
   4.50  15.50  10.50
   4.50  16.00  11.00
   4.50  16.50  11.00
   4.50  17.00  11.50
 cfdata: END --- >


 ssidat: < --- BEGIN
 alpha_Fo  alpha_Fi  eta_Fo
   0.63   0.54   1.00
 eta_reb  alpha_d_su  iplug_vmode  vmax_user
   0.50   0.50    1   0.00
 eta_amh  eta_bmh  eta_phimh
   1.00   1.00   1.00
 ssidat: END --- >


 chndat: < --- BEGIN
 iscope_Bw  l_fac_Bw  eta_Vst_wall  delta_Bw_user  Bw_caisson_user
    1    1.00        1.00        0.00        0.00    
 dtheta_lug_deg  psi_twist_deg
    0.00        0.00    
 chndat: END --- >


 ldata__anchor: < --- BEGIN
 nlc   nlfac_T
 10  1
 ldata__anchor: theta_lug  (l_facT) ***
    0.00        1.00       ! ? missing text
    10.0        1.00       ! ? missing text
    20.0        1.00       ! ? missing text
    30.0        1.00       ! ? missing text
    40.0        1.00       ! ? missing text
    50.0        1.00       ! ? missing text
    60.0        1.00       ! ? missing text
    70.0        1.00       ! ? missing text
    80.0        1.00       ! ? missing text
    90.0        1.00       ! ? missing text
 ldata__anchor: END --- >


 mcdata: < --- BEGIN
 ioutd  ioute
    3   -2
 eps_int  jmax_int  jmin_int
   0.100E-03 15  5
 mcdata: END --- >

 datain_caisson: END --- >


clen_theoretical_sub: < --- BEGIN
clen_theoretical_sub: no theoretical caisson L values for FACTORED VMH load;
clen_theoretical_sub: can't find L without VHload (MODE_VHM = 16, 17, 22 and 23).
clen_theoretical_sub: END --- >



caisson_vhm: nlines_warnings :    5
caisson_vhm: nlines_errors   :    0

WARNING: gmdata. soil layer # 4; BDEN=5.00 kN/m^3 is inconsistent with SU_BOT=41.00 kPa.
WARNING. cfdata: NCGEOM > 1 with offset lug implies variable ZLUG*. [?IRO_LUG=0].
WARNING. ldata__anchor: ILC =    1; THETA_LUG_DEG = 0. [horizontal chain inclination at lug level].
WARNING. ldata__anchor: ILC =   10; THETA_LUG_DEG = 90. [vertical chain inclination at lug level].
WARNING. ldata__anchor: ILC =   10; THETA_LUG_DEG = 90 & IRO_LUG > 0. [ZLUG_CL at infinite depth].

solve_MODE22_sub: < --- BEGIN

  VHM load case #=    1; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5322.815
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000       0.000
   zlug_cL                               [m]:      10.000
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5322.815
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    -548.032    5322.815  -53228.147
   Vstar,Hstar,Mstar                     [-]:      -0.286      10.962      -7.308
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.962      -7.308      -0.286
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.990
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.001
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.3021318E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    2; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5327.700
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      10.000
   zlug_cL                               [m]:      10.397
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:     925.145
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5246.760
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:     377.113    5246.760  -54549.177
   Vstar,Hstar,Mstar                     [-]:       0.197      10.806      -7.490
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.806      -7.490       0.197
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.986
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.011
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.997
 > f_VHM_fun                             [-]: -0.5849528E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    3; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5088.157
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      20.000
   zlug_cL                               [m]:      10.819
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1740.252
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4781.303
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1192.220    4781.303  -51728.601
   Vstar,Hstar,Mstar                     [-]:       0.622       9.847      -7.102
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.847      -7.102       0.622
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.840
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.055
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.895
 > f_VHM_fun                             [-]:  0.3193251E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    4; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4402.902
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      30.000
   zlug_cL                               [m]:      11.299
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2201.451
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3813.025
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1653.419    3813.025  -43083.515
   Vstar,Hstar,Mstar                     [-]:       0.863       7.853      -5.915
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.853      -5.915       0.863
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.550
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.097
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.647
 > f_VHM_fun                             [-]:  0.5997811E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    5; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3686.213
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      40.000
   zlug_cL                               [m]:      11.888
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2369.452
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2823.803
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1821.420    2823.803  -33569.301
   Vstar,Hstar,Mstar                     [-]:       0.950       5.816      -4.609
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.816      -4.609       0.950
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.312
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.118
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.430
 > f_VHM_fun                             [-]:  0.3124337E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00003
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    6; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3165.113
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      50.000
   zlug_cL                               [m]:      12.681
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2424.617
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2034.495
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1876.585    2034.495  -25800.344
   Vstar,Hstar,Mstar                     [-]:       0.979       4.190      -3.542
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  4.190      -3.542       0.979
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.170
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.128
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.297
 > f_VHM_fun                             [-]: -0.1114777E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    7; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2822.911
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      60.000
   zlug_cL                               [m]:      13.897
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2444.712
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1411.455
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1896.680    1411.455  -19615.156
   Vstar,Hstar,Mstar                     [-]:       0.989       2.907      -2.693
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.907      -2.693       0.989
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.087
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.133
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.220
 > f_VHM_fun                             [-]:  0.5203263E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00052
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    8; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2609.181
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      70.000
   zlug_cL                               [m]:      16.182
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2451.828
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     892.392
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1903.796     892.392  -14440.537
   Vstar,Hstar,Mstar                     [-]:       0.993       1.838      -1.983
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.838      -1.983       0.993
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.040
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.136
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.182
 > f_VHM_fun                             [-]: -0.5749094E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00575
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    9; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2494.176
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      80.000
   zlug_cL                               [m]:      22.760
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2456.284
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     433.109
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1908.252     433.109   -9857.731
   Vstar,Hstar,Mstar                     [-]:       0.996       0.892      -1.353
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.892      -1.353       0.996
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.013
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.139
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.151
 > f_VHM_fun                             [-]:  0.8670851E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00087
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=   10; caisson geometry #=    1

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2457.239
   L , D                                 [m]:      15.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.000      90.000
   zlug_cL                               [m]:************
   Bw , Bw_plug                         [kN]:     548.032       0.000
   su_av_L                             [kPa]:       7.193
   Vmax                                 [kN]:    1916.844
   Hfac=L   D su_av_L                   [kN]:     485.559
   Mfac=L^2 D su_av_L                  [kNm]:    7283.385
   aMH , bMH                             [-]:      13.238       1.675
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2457.239
   Hlug=Tlug*cos(theta_lug_star)        [kN]:       0.000
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1909.207       0.000   -5528.787
   Vstar,Hstar,Mstar                     [-]:       0.996       0.000      -0.759
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.000      -0.759       0.996
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.238       1.675     -33.949
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.238       1.675     -33.949
   aVH , bVH                             [-]:       4.501       3.182
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.001
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.141
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.143
 > f_VHM_fun                             [-]: -0.9364984E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00094
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.19    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      967.12170
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      810.88121
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.33    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.3    
   qv_tip = Nc * su_av_tip             [kPa]     119.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    950.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1916.84405
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1778.00291
   Qleaking   = Fo                      [kN]:      967.12170
 > Vmax_fun                             [kN]:     1916.84405
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.39    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.18    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      548.03197
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    1; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5637.288
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500       0.000
   zlug_cL                               [m]:      10.500
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5637.288
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    -564.526    5637.288  -59191.519
   Vstar,Hstar,Mstar                     [-]:      -0.282      10.967      -7.430
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                 10.967      -7.430      -0.282
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.991
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.000
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.3036180E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    2; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5602.994
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      10.000
   zlug_cL                               [m]:      10.897
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:     972.950
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5517.872
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:     408.424    5517.872  -60126.796
   Vstar,Hstar,Mstar                     [-]:       0.204      10.735      -7.547
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                 10.735      -7.547       0.204
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.972
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.025
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.997
 > f_VHM_fun                             [-]: -0.6198103E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    3; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5318.014
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      20.000
   zlug_cL                               [m]:      11.319
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1818.868
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4997.298
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1254.342    4997.298  -56564.083
   Vstar,Hstar,Mstar                     [-]:       0.627       9.722      -7.100
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  9.722      -7.100       0.627
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.818
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.075
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.892
 > f_VHM_fun                             [-]:  0.2836026E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    4; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4589.803
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      30.000
   zlug_cL                               [m]:      11.799
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2294.901
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3974.886
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1730.376    3974.886  -46899.828
   Vstar,Hstar,Mstar                     [-]:       0.866       7.733      -5.887
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  7.733      -5.887       0.866
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.532
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.113
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.644
 > f_VHM_fun                             [-]:  0.4691745E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    5; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3839.717
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      40.000
   zlug_cL                               [m]:      12.388
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2468.123
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2941.394
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1903.597    2941.394  -36437.915
   Vstar,Hstar,Mstar                     [-]:       0.952       5.723      -4.574
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  5.723      -4.574       0.952
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.301
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.127
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.428
 > f_VHM_fun                             [-]:  0.2045384E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00002
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    6; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3295.663
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      50.000
   zlug_cL                               [m]:      13.181
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2524.624
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2118.411
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1960.099    2118.411  -27923.721
   Vstar,Hstar,Mstar                     [-]:       0.980       4.121      -3.505
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  4.121      -3.505       0.980
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.163
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.130
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.293
 > f_VHM_fun                             [-]: -0.1194278E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    7; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2937.357
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      60.000
   zlug_cL                               [m]:      14.397
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2543.826
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1468.679
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1979.300    1468.679  -21144.733
   Vstar,Hstar,Mstar                     [-]:       0.990       2.857      -2.654
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  2.857      -2.654       0.990
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.084
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.130
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.219
 > f_VHM_fun                             [-]: -0.5301436E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00530
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    8; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2716.848
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      70.000
   zlug_cL                               [m]:      16.682
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2553.002
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     929.217
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1988.476     929.217  -15501.029
   Vstar,Hstar,Mstar                     [-]:       0.995       1.808      -1.946
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  1.808      -1.946       0.995
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.038
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.130
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.168
 > f_VHM_fun                             [-]: -0.3043504E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00030
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    9; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2595.777
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      80.000
   zlug_cL                               [m]:      23.260
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2556.342
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     450.752
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1991.816     450.752  -10484.665
   Vstar,Hstar,Mstar                     [-]:       0.996       0.877      -1.316
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  0.877      -1.316       0.996
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.012
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.129
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.142
 > f_VHM_fun                             [-]: -0.1812424E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00181
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=   10; caisson geometry #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2557.945
   L , D                                 [m]:      15.500       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      90.000
   zlug_cL                               [m]:************
   Bw , Bw_plug                         [kN]:     564.526       0.000
   su_av_L                             [kPa]:       7.369
   Vmax                                 [kN]:    1999.174
   Hfac=L   D su_av_L                   [kN]:     514.002
   Mfac=L^2 D su_av_L                  [kNm]:    7967.030
   aMH , bMH                             [-]:      13.304       1.678
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2557.945
   Hlug=Tlug*cos(theta_lug_star)        [kN]:       0.000
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1993.420       0.000   -5755.377
   Vstar,Hstar,Mstar                     [-]:       0.997       0.000      -0.722
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.50
   X = Hstar; Y = Mstar; Z = Vstar                  0.000      -0.722       0.997
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.304       1.678     -33.958
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.304       1.678     -33.958
   aVH , bVH                             [-]:       4.577       3.154
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.001
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.127
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.128
 > f_VHM_fun                             [-]:  0.4107825E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00041
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  15.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.37    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1023.77353
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      858.38082
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.44    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    13.6    
   qv_tip = Nc * su_av_tip             [kPa]     123.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:    975.    
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     1999.17376
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1882.15436
   Qleaking   = Fo                      [kN]:     1023.77353
 > Vmax_fun                             [kN]:     1999.17376
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.63    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.43    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      564.52550
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  15.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    1; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5945.141
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000       0.000
   zlug_cL                               [m]:      11.000
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5945.141
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    -581.019    5945.141  -65396.547
   Vstar,Hstar,Mstar                     [-]:      -0.279      10.943      -7.524
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.943      -7.524      -0.279
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.986
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.006
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.3068570E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    2; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5874.219
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      10.000
   zlug_cL                               [m]:      11.397
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1020.047
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5784.976
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:     439.028    5784.976  -65929.842
   Vstar,Hstar,Mstar                     [-]:       0.211      10.649      -7.585
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.649      -7.585       0.211
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.955
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.041
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.997
 > f_VHM_fun                             [-]: -0.6540893E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    3; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5548.174
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      20.000
   zlug_cL                               [m]:      11.819
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1897.587
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5213.578
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1316.568    5213.578  -61618.930
   Vstar,Hstar,Mstar                     [-]:       0.632       9.597      -7.089
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.597      -7.089       0.632
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.795
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.095
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.890
 > f_VHM_fun                             [-]:  0.2470320E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    4; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4779.736
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      30.000
   zlug_cL                               [m]:      12.299
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2389.868
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4139.373
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1808.849    4139.373  -50910.304
   Vstar,Hstar,Mstar                     [-]:       0.868       7.620      -5.857
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.620      -5.857       0.868
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.515
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.128
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.642
 > f_VHM_fun                             [-]:  0.3649115E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    5; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3996.096
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      40.000
   zlug_cL                               [m]:      12.888
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2568.641
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3061.187
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1987.622    3061.187  -39452.496
   Vstar,Hstar,Mstar                     [-]:       0.954       5.635      -4.539
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.635      -4.539       0.954
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.291
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.134
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.425
 > f_VHM_fun                             [-]:  0.1090986E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    6; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3428.479
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      50.000
   zlug_cL                               [m]:      13.681
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2626.367
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2203.784
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2045.348    2203.784  -30150.947
   Vstar,Hstar,Mstar                     [-]:       0.982       4.057      -3.469
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  4.057      -3.469       0.982
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.157
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.132
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.289
 > f_VHM_fun                             [-]: -0.1983534E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00002
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    7; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3056.229
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      60.000
   zlug_cL                               [m]:      14.897
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2646.772
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1528.115
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2065.753    1528.115  -22764.498
   Vstar,Hstar,Mstar                     [-]:       0.992       2.813      -2.619
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.813      -2.619       0.992
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.081
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.128
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.208
 > f_VHM_fun                             [-]:  0.5609160E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00006
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    8; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2824.244
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      70.000
   zlug_cL                               [m]:      17.182
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2653.921
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     965.948
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2072.902     965.948  -16596.755
   Vstar,Hstar,Mstar                     [-]:       0.995       1.778      -1.909
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.778      -1.909       0.995
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.036
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.123
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.166
 > f_VHM_fun                             [-]: -0.6769518E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00677
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    9; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2699.217
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      80.000
   zlug_cL                               [m]:      23.760
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2658.210
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     468.714
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2077.191     468.714  -11136.828
   Vstar,Hstar,Mstar                     [-]:       0.997       0.863      -1.281
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.863      -1.281       0.997
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.011
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.119
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.132
 > f_VHM_fun                             [-]: -0.1087443E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00109
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=   10; caisson geometry #=    3

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2659.153
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      90.000
   zlug_cL                               [m]:************
   Bw , Bw_plug                         [kN]:     581.019       0.000
   su_av_L                             [kPa]:       7.545
   Vmax                                 [kN]:    2083.163
   Hfac=L   D su_av_L                   [kN]:     543.259
   Mfac=L^2 D su_av_L                  [kNm]:    8692.144
   aMH , bMH                             [-]:      13.371       1.682
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2659.153
   Hlug=Tlug*cos(theta_lug_star)        [kN]:       0.000
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2078.134       0.000   -5983.094
   Vstar,Hstar,Mstar                     [-]:       0.998       0.000      -0.688
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.000      -0.688       0.998
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.001
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.115
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.122
 > f_VHM_fun                             [-]: -0.6336318E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00634
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.55    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1082.04686
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      907.23997
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.56    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.0    
   qv_tip = Nc * su_av_tip             [kPa]     126.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.100E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2083.16349
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1989.28683
   Qleaking   = Fo                      [kN]:     1082.04686
 > Vmax_fun                             [kN]:     2083.16349
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    7.88    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.67    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      581.01903
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    1; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6380.324
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000       0.000
   zlug_cL                               [m]:      11.000
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6380.324
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    -597.513    6380.324  -70183.559
   Vstar,Hstar,Mstar                     [-]:      -0.275      11.129      -7.419
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                 11.129      -7.419      -0.275
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.991
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.002
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.2977093E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    2; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6394.381
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      10.000
   zlug_cL                               [m]:      11.397
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1110.373
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6297.236
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:     512.860    6297.236  -71767.931
   Vstar,Hstar,Mstar                     [-]:       0.236      10.984      -7.587
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                 10.984      -7.587       0.236
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.987
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.008
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.995
 > f_VHM_fun                             [-]: -0.7083836E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    3; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6033.130
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      20.000
   zlug_cL                               [m]:      11.819
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2063.452
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5669.288
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1465.940    5669.288  -67004.937
   Vstar,Hstar,Mstar                     [-]:       0.676       9.889      -7.083
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  9.889      -7.083       0.676
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.819
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.043
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.862
 > f_VHM_fun                             [-]:  0.4468888E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    4; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5097.819
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      30.000
   zlug_cL                               [m]:      12.299
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2548.910
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4414.841
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1951.397    4414.841  -54298.299
   Vstar,Hstar,Mstar                     [-]:       0.900       7.701      -5.740
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  7.701      -5.740       0.900
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.510
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.074
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.583
 > f_VHM_fun                             [-]: -0.8811528E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00009
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    5; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4199.118
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      40.000
   zlug_cL                               [m]:      12.888
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2699.141
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3216.711
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2101.628    3216.711  -41456.886
   Vstar,Hstar,Mstar                     [-]:       0.969       5.611      -4.383
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  5.611      -4.383       0.969
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.279
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.088
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.367
 > f_VHM_fun                             [-]:  0.2364591E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00002
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    6; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3578.950
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      50.000
   zlug_cL                               [m]:      13.681
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2741.635
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2300.505
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2144.122    2300.505  -31474.231
   Vstar,Hstar,Mstar                     [-]:       0.988       4.013      -3.327
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  4.013      -3.327       0.988
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.149
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.094
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.244
 > f_VHM_fun                             [-]: -0.2791748E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00028
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    7; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3181.758
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      60.000
   zlug_cL                               [m]:      14.897
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2755.483
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1590.879
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2157.970    1590.879  -23699.504
   Vstar,Hstar,Mstar                     [-]:       0.995       2.775      -2.505
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  2.775      -2.505       0.995
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.076
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.098
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.174
 > f_VHM_fun                             [-]:  0.1246824E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00012
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    8; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2937.920
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      70.000
   zlug_cL                               [m]:      17.182
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2760.742
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1004.828
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2163.229    1004.828  -17264.775
   Vstar,Hstar,Mstar                     [-]:       0.997       1.753      -1.825
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  1.753      -1.825       0.997
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.034
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.101
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.133
 > f_VHM_fun                             [-]:  0.1639812E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00164
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    9; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2804.617
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      80.000
   zlug_cL                               [m]:      23.760
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2762.009
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     487.017
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2164.496     487.017  -11571.702
   Vstar,Hstar,Mstar                     [-]:       0.998       0.849      -1.223
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  0.849      -1.223       0.998
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.011
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.103
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.120
 > f_VHM_fun                             [-]: -0.6591410E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00659
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=   10; caisson geometry #=    4

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2762.425
   L , D                                 [m]:      16.500       4.500
   zlug , theta_lug_star           [m] [deg]:      11.000      90.000
   zlug_cL                               [m]:************
   Bw , Bw_plug                         [kN]:     597.513       0.000
   su_av_L                             [kPa]:       7.721
   Vmax                                 [kN]:    2169.121
   Hfac=L   D su_av_L                   [kN]:     573.311
   Mfac=L^2 D su_av_L                  [kNm]:    9459.623
   aMH , bMH                             [-]:      13.438       1.685
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2762.425
   Hlug=Tlug*cos(theta_lug_star)        [kN]:       0.000
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2164.912       0.000   -6215.456
   Vstar,Hstar,Mstar                     [-]:       0.998       0.000      -0.657
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.50
   X = Hstar; Y = Mstar; Z = Vstar                  0.000      -0.657       0.998
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.438       1.685     -33.970
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.438       1.685     -33.970
   aVH , bVH                             [-]:       4.737       3.095
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.001
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.105
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.115
 > f_VHM_fun                             [-]: -0.9902064E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00990
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  16.50   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.72    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1141.90253
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      957.42583
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.67    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.4    
   qv_tip = Nc * su_av_tip             [kPa]     129.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.103E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2169.12073
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2099.32836
   Qleaking   = Fo                      [kN]:     1141.90253
 > Vmax_fun                             [kN]:     2169.12073
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.12    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    8.92    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      597.51256
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  16.50   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    1; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6732.452
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500       0.000
   zlug_cL                               [m]:      11.500
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6732.452
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    -614.006    6732.452  -77423.197
   Vstar,Hstar,Mstar                     [-]:      -0.272      11.143      -7.538
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                 11.143      -7.538      -0.272
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.992
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.000
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.2991364E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    2; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6705.200
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      10.000
   zlug_cL                               [m]:      11.897
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1164.346
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6603.333
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:     550.340    6603.333  -78558.112
   Vstar,Hstar,Mstar                     [-]:       0.244      10.929      -7.648
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.929      -7.648       0.244
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.975
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.019
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.994
 > f_VHM_fun                             [-]: -0.7542048E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    3; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6288.926
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      20.000
   zlug_cL                               [m]:      12.319
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2150.939
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5909.657
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1536.933    5909.657  -72800.673
   Vstar,Hstar,Mstar                     [-]:       0.681       9.781      -7.088
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.781      -7.088       0.681
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.799
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.059
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.858
 > f_VHM_fun                             [-]:  0.3987029E-06
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00000
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    4; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5300.446
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      30.000
   zlug_cL                               [m]:      12.799
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2650.223
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4590.321
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2036.217    4590.321  -58751.690
   Vstar,Hstar,Mstar                     [-]:       0.902       7.597      -5.720
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.597      -5.720       0.902
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.494
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.087
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.581
 > f_VHM_fun                             [-]: -0.7302168E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00007
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    5; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4362.149
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      40.000
   zlug_cL                               [m]:      13.388
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2803.935
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3341.600
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2189.929    3341.600  -44737.254
   Vstar,Hstar,Mstar                     [-]:       0.970       5.531      -4.356
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.531      -4.356       0.970
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.270
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.095
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.366
 > f_VHM_fun                             [-]: -0.1245333E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    6; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3716.533
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      50.000
   zlug_cL                               [m]:      14.181
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2847.030
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2388.942
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2233.024    2388.942  -33878.645
   Vstar,Hstar,Mstar                     [-]:       0.989       3.954      -3.298
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  3.954      -3.298       0.989
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.144
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.097
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.241
 > f_VHM_fun                             [-]: -0.8572406E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00009
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    7; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3303.413
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      60.000
   zlug_cL                               [m]:      15.397
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2860.839
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1651.706
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2246.833    1651.706  -25431.512
   Vstar,Hstar,Mstar                     [-]:       0.995       2.734      -2.476
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.734      -2.476       0.995
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.073
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.097
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.170
 > f_VHM_fun                             [-]:  0.2293949E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00023
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    8; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3048.881
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      70.000
   zlug_cL                               [m]:      17.682
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2865.011
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1042.779
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2251.005    1042.779  -18438.231
   Vstar,Hstar,Mstar                     [-]:       0.997       1.726      -1.795
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.726      -1.795       0.997
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.032
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.096
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.137
 > f_VHM_fun                             [-]: -0.8131247E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00813
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=    9; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2912.002
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      80.000
   zlug_cL                               [m]:      24.260
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2867.762
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     505.664
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2253.756     505.664  -12267.598
   Vstar,Hstar,Mstar                     [-]:       0.998       0.837      -1.194
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.837      -1.194       0.998
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.010
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.096
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.107
 > f_VHM_fun                             [-]: -0.1133695E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00113
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


  VHM load case #=   10; caisson geometry #=    5

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2868.557
   L , D                                 [m]:      17.000       4.500
   zlug , theta_lug_star           [m] [deg]:      11.500      90.000
   zlug_cL                               [m]:************
   Bw , Bw_plug                         [kN]:     614.006       0.000
   su_av_L                             [kPa]:       7.898
   Vmax                                 [kN]:    2257.155
   Hfac=L   D su_av_L                   [kN]:     604.202
   Mfac=L^2 D su_av_L                  [kNm]:   10271.428
   aMH , bMH                             [-]:      13.506       1.688
   phiMH , phiMH                 [rad] [deg]:      -0.593     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2868.557
   Hlug=Tlug*cos(theta_lug_star)        [kN]:       0.000
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    2254.551       0.000   -6454.253
   Vstar,Hstar,Mstar                     [-]:       0.999       0.000      -0.628
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  17.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.000      -0.628       0.999
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.506       1.688     -33.976
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.506       1.688     -33.976
   aVH , bVH                             [-]:       4.818       3.065
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.001
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.095
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.096
 > f_VHM_fun                             [-]: -0.9874570E-05
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00001
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  17.00   4.50

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.63400
 > alpha_Fo_twist                        [-]:     0.63400
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  0.500
   wt_c = D * wt_D_side                  [m]:   0.04
   wt_x = wt_c                           [m]:   0.04
   Di = D - 2 * wt_c                     [m]:   4.43
   su_av_L   = av 0    to L            [kPa]:    7.90    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1203.43051
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1009.01385
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    3.78    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    9.00    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    14.7    
   qv_tip = Nc * su_av_tip             [kPa]     133.    
   Abase = pi * D * D / 4              [m^2]:    15.9    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.105E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     2257.15472
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2212.44436
   Qleaking   = Fo                      [kN]:     1203.43051
 > Vmax_fun                             [kN]:     2257.15472
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < iscope_Bw                             [-]:  1
   wt_D_side                             [-]:  0.008
   wt_D_top                              [-]:  0.011
   wt_c = D * wt_D_side                  [m]:  0.035
   wt_x = wt_c                           [m]:  0.035
   wt_t = D * wt_D_top                   [m]:  0.050
   Di = D - 2 * wt_c                     [m]:  4.430
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.492    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    15.9    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.37    
   Vst_t =   Atop          * wt_t      [m^3]:   0.794    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.16    
   gamma_sub_steel                  [kN/m^3]:    67.0    
   DELTA_BW_USER                        [kN]:    0.00    
   Bw_caisson = gamma_sub_steel * Vst + delta_Bw_user
 > Bw_caisson_fun                       [kN]:      614.00608
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  17.00   4.50
 < wt_D_side (= WT / D)                  [-]:  0.008
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >



 -----------------------------------------------
 solve_MODE22_sub: CAISSON RESISTANCES & WEIGHTS
 MODE_VHM, problem solution mode =   22
 IPLUG_VMODE, axial capacity mode  =  1
 ISCOPE_BW, caisson weight BW mode =  1
 ilc    = VHM load case #            
 icgeom = caisson geometry #         
 D    = caisson outer diameter       
 L    = caisson embedded length      
 L/D  = caisson embedment ratio      
 Vmax = caisson axial resistance     
 Hmax = caisson FIXED HEAD lateral resistance 
 H0   = caisson FREE  HEAD lateral resistance 
 Bw   = caisson submerged weight (only used for anchor foundations)
 Bw*  = caisson+soil plug submerged weight (only for IPLUG_VMODE=5)
 su_av_L = soil average su between caisson head (seafloor) and tip (L)
 ----------------------------------------------------------------------------------------
  ilc       D      L      L/D       Vmax        Hmax         H0          Bw       su_av_L
   icgeom  [m]    [m]     [-]       [kN]        [kN]        [kN]        [kN]        [kPa]
 ----------------------------------------------------------------------------------------
    1  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    1  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    1  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    1  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    1  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    2  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    2  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    2  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    2  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    2  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    3  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    3  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    3  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    3  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    3  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    4  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    4  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    4  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    4  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    4  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    5  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    5  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    5  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    5  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    5  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    6  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    6  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    6  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    6  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    6  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    7  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    7  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    7  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    7  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    7  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    8  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    8  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    8  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    8  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    8  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

    9  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    9  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
    9  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
    9  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
    9  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9

   10  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
   10  2   4.50  15.50   3.44      1999.2      5672.1      1544.3       564.5         7.4
   10  3   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
   10  4   4.50  16.50   3.67      2169.1      6389.3      1728.7       597.5         7.7
   10  5   4.50  17.00   3.78      2257.2      6767.3      1825.2       614.0         7.9
 ----------------------------------------------------------------------------------------
  ilc       D      L      L/D       Vmax        Hmax         H0          Bw       su_av_L
   icgeom  [m]    [m]     [-]       [kN]        [kN]        [kN]        [kN]        [kPa]
 ----------------------------------------------------------------------------------------


 ------------------------------------
 solve_MODE22_sub: SUMMARY OF RESULTS
 ilc    = VHM load case #            
 icgeom = caisson geometry #         
 D      = caisson outer diameter           [m] 
 L      = caisson embedded length          [m] 
 zlug   = caisson lug level                [m] 
 theta_lug = load inclination            [deg] 
 Tlug      = UNFACTORED anchor chain load [kN] 
 Bw        = caisson buoyant weight       [kN] 
 iters     = # iterations                  [-] 
 f_VHM     = VHM yield function            [-] 
 -----------------------------------------------------------------------
 ilc        D      L    zlug  theta    Tlug     Bw    ( iters    f_VHM )
  icgeom   [m]    [m]   [m]   [deg]    [kN]    [kN]   ( [-]      [-]   )
 -----------------------------------------------------------------------
    1  1   4.50  15.00  10.00  0.00   5322.8   548.0       5  -0.302E-05   ! ? missing text
    1  2   4.50  15.50  10.50  0.00   5637.3   564.5       5  -0.304E-05   ! ? missing text
    1  3   4.50  16.00  11.00  0.00   5945.1   581.0       5  -0.307E-05   ! ? missing text
    1  4   4.50  16.50  11.00  0.00   6380.3   597.5       5  -0.298E-05   ! ? missing text
    1  5   4.50  17.00  11.50  0.00   6732.5   614.0       5  -0.299E-05   ! ? missing text

    2  1   4.50  15.00  10.00 10.00   5327.7   548.0       5  -0.585E-05   ! ? missing text
    2  2   4.50  15.50  10.50 10.00   5603.0   564.5       5  -0.620E-05   ! ? missing text
    2  3   4.50  16.00  11.00 10.00   5874.2   581.0       5  -0.654E-05   ! ? missing text
    2  4   4.50  16.50  11.00 10.00   6394.4   597.5       5  -0.708E-05   ! ? missing text
    2  5   4.50  17.00  11.50 10.00   6705.2   614.0       5  -0.754E-05   ! ? missing text

    3  1   4.50  15.00  10.00 20.00   5088.2   548.0       6   0.319E-06   ! ? missing text
    3  2   4.50  15.50  10.50 20.00   5318.0   564.5       6   0.284E-06   ! ? missing text
    3  3   4.50  16.00  11.00 20.00   5548.2   581.0       6   0.247E-06   ! ? missing text
    3  4   4.50  16.50  11.00 20.00   6033.1   597.5       6   0.447E-06   ! ? missing text
    3  5   4.50  17.00  11.50 20.00   6288.9   614.0       6   0.399E-06   ! ? missing text

    4  1   4.50  15.00  10.00 30.00   4402.9   548.0       6   0.600E-06   ! ? missing text
    4  2   4.50  15.50  10.50 30.00   4589.8   564.5       6   0.469E-06   ! ? missing text
    4  3   4.50  16.00  11.00 30.00   4779.7   581.0       6   0.365E-06   ! ? missing text
    4  4   4.50  16.50  11.00 30.00   5097.8   597.5       5  -0.881E-04   ! ? missing text
    4  5   4.50  17.00  11.50 30.00   5300.4   614.0       5  -0.730E-04   ! ? missing text

    5  1   4.50  15.00  10.00 40.00   3686.2   548.0       5   0.312E-04   ! ? missing text
    5  2   4.50  15.50  10.50 40.00   3839.7   564.5       5   0.205E-04   ! ? missing text
    5  3   4.50  16.00  11.00 40.00   3996.1   581.0       5   0.109E-04   ! ? missing text
    5  4   4.50  16.50  11.00 40.00   4199.1   597.5       4   0.236E-04   ! ? missing text
    5  5   4.50  17.00  11.50 40.00   4362.1   614.0       5  -0.125E-04   ! ? missing text

    6  1   4.50  15.00  10.00 50.00   3165.1   548.0       8  -0.111E-04   ! ? missing text
    6  2   4.50  15.50  10.50 50.00   3295.7   564.5       8  -0.119E-04   ! ? missing text
    6  3   4.50  16.00  11.00 50.00   3428.5   581.0       8  -0.198E-04   ! ? missing text
    6  4   4.50  16.50  11.00 50.00   3579.0   597.5       5  -0.279E-03   ! ? missing text
    6  5   4.50  17.00  11.50 50.00   3716.5   614.0       6  -0.857E-04   ! ? missing text

    7  1   4.50  15.00  10.00 60.00   2822.9   548.0       6   0.520E-03   ! ? missing text
    7  2   4.50  15.50  10.50 60.00   2937.4   564.5       8  -0.530E-02   ! ? missing text
    7  3   4.50  16.00  11.00 60.00   3056.2   581.0      10   0.561E-04   ! ? missing text
    7  4   4.50  16.50  11.00 60.00   3181.8   597.5      10   0.125E-03   ! ? missing text
    7  5   4.50  17.00  11.50 60.00   3303.4   614.0      10   0.229E-03   ! ? missing text

    8  1   4.50  15.00  10.00 70.00   2609.2   548.0       8  -0.575E-02   ! ? missing text
    8  2   4.50  15.50  10.50 70.00   2716.8   564.5       9  -0.304E-03   ! ? missing text
    8  3   4.50  16.00  11.00 70.00   2824.2   581.0       8  -0.677E-02   ! ? missing text
    8  4   4.50  16.50  11.00 70.00   2937.9   597.5      11   0.164E-02   ! ? missing text
    8  5   4.50  17.00  11.50 70.00   3048.9   614.0      10  -0.813E-02   ! ? missing text

    9  1   4.50  15.00  10.00 80.00   2494.2   548.0       8   0.867E-03   ! ? missing text
    9  2   4.50  15.50  10.50 80.00   2595.8   564.5       8  -0.181E-02   ! ? missing text
    9  3   4.50  16.00  11.00 80.00   2699.2   581.0       8  -0.109E-02   ! ? missing text
    9  4   4.50  16.50  11.00 80.00   2804.6   597.5      10  -0.659E-02   ! ? missing text
    9  5   4.50  17.00  11.50 80.00   2912.0   614.0       8  -0.113E-02   ! ? missing text

   10  1   4.50  15.00  10.00 90.00   2457.2   548.0       8  -0.936E-03   ! ? missing text
   10  2   4.50  15.50  10.50 90.00   2557.9   564.5       8   0.411E-03   ! ? missing text
   10  3   4.50  16.00  11.00 90.00   2659.2   581.0      10  -0.634E-02   ! ? missing text
   10  4   4.50  16.50  11.00 90.00   2762.4   597.5       6  -0.990E-02   ! ? missing text
   10  5   4.50  17.00  11.50 90.00   2868.6   614.0      24  -0.987E-05   ! ? missing text
 -----------------------------------------------------------------------
 ilc        D      L    zlug  theta    Tlug     Bw    ( iters    f_VHM )
  icgeom   [m]    [m]   [m]   [deg]    [kN]    [kN]   ( [-]      [-]   )
 -----------------------------------------------------------------------

VHlug_resist_sub: < --- BEGIN
  load case #=    1; caisson geometry #=    1 (#rows results= =  181)
  L         [m] =   15.00
  D         [m] =    4.50
  zlug      [m] =   10.00
  iro_lug   [-] =   1: offset + D/2 (lug on outer face)
  m_fac     [-] =   1.300
  Hmax     [kN] =    0.533E+04
  Vmax     [kN] =    0.192E+04
  theta*        = resistance inclination at lug
  Vlug_theta*, Hlug_theta*
                = corresponding VH FACTORED resistances
  T_theta*      = sqrt( Vlug_theta*^2 + Hlug_theta*^2)
------------------------------------------------------------------------------
 theta*     Vlug_theta*  Hlug_theta*  T_theta*   Vlug_theta*  Hlug_theta*  row
  [deg]        [kN]         [kN]        [kN]      / Vmax [-]   / Hmax [-]  [-]
------------------------------------------------------------------------------
    90.0       0.191E+04   0.117E-12   0.191E+04       0.999    0.000        1
    89.0       0.191E+04    33.4       0.191E+04       0.999    0.006        2
    88.0       0.191E+04    66.9       0.192E+04       0.999    0.013        3
    87.0       0.191E+04    100.       0.192E+04       0.999    0.019        4
    86.0       0.191E+04    134.       0.192E+04       0.999    0.025        5
    85.0       0.191E+04    167.       0.192E+04       0.999    0.031        6
    84.0       0.191E+04    201.       0.192E+04       0.999    0.038        7
    83.0       0.191E+04    235.       0.193E+04       0.999    0.044        8
    82.0       0.191E+04    269.       0.193E+04       0.999    0.050        9
    81.0       0.191E+04    303.       0.194E+04       0.999    0.057       10
    80.0       0.191E+04    337.       0.194E+04       0.999    0.063       11
    79.0       0.191E+04    372.       0.195E+04       0.998    0.070       12
    78.0       0.191E+04    407.       0.196E+04       0.998    0.076       13
    77.0       0.191E+04    442.       0.196E+04       0.998    0.083       14
    76.0       0.191E+04    477.       0.197E+04       0.998    0.089       15
    75.0       0.191E+04    513.       0.198E+04       0.998    0.096       16
    74.0       0.191E+04    549.       0.199E+04       0.998    0.103       17
    73.0       0.191E+04    585.       0.200E+04       0.998    0.110       18
    72.0       0.191E+04    622.       0.201E+04       0.998    0.117       19
    71.0       0.191E+04    659.       0.202E+04       0.998    0.124       20
    70.0       0.191E+04    696.       0.204E+04       0.998    0.131       21
    69.0       0.191E+04    734.       0.205E+04       0.998    0.138       22
    68.0       0.191E+04    772.       0.206E+04       0.997    0.145       23
    67.0       0.191E+04    812.       0.208E+04       0.998    0.152       24
    66.0       0.191E+04    851.       0.209E+04       0.998    0.160       25
    65.0       0.191E+04    891.       0.211E+04       0.997    0.167       26
    64.0       0.191E+04    932.       0.213E+04       0.997    0.175       27
    63.0       0.191E+04    974.       0.215E+04       0.997    0.183       28
    62.0       0.191E+04   0.102E+04   0.216E+04       0.997    0.190       29
    61.0       0.191E+04   0.106E+04   0.218E+04       0.997    0.199       30
    60.0       0.191E+04   0.110E+04   0.221E+04       0.997    0.207       31
    59.0       0.191E+04   0.115E+04   0.223E+04       0.996    0.215       32
    58.0       0.191E+04   0.119E+04   0.225E+04       0.996    0.224       33
    57.0       0.191E+04   0.124E+04   0.228E+04       0.996    0.232       34
    56.0       0.191E+04   0.129E+04   0.230E+04       0.995    0.241       35
    55.0       0.191E+04   0.134E+04   0.233E+04       0.995    0.251       36
    54.0       0.191E+04   0.139E+04   0.236E+04       0.995    0.260       37
    53.0       0.191E+04   0.144E+04   0.239E+04       0.995    0.269       38
    52.0       0.191E+04   0.149E+04   0.242E+04       0.994    0.279       39
    51.0       0.190E+04   0.154E+04   0.245E+04       0.994    0.289       40
    50.0       0.190E+04   0.160E+04   0.248E+04       0.993    0.300       41
    49.0       0.190E+04   0.165E+04   0.252E+04       0.992    0.310       42
    48.0       0.190E+04   0.171E+04   0.256E+04       0.992    0.321       43
    47.0       0.190E+04   0.177E+04   0.260E+04       0.991    0.332       44
    46.0       0.190E+04   0.183E+04   0.264E+04       0.990    0.344       45
    45.0       0.190E+04   0.190E+04   0.268E+04       0.989    0.356       46
    44.0       0.189E+04   0.196E+04   0.273E+04       0.988    0.368       47
    43.0       0.189E+04   0.203E+04   0.277E+04       0.987    0.381       48
    42.0       0.189E+04   0.210E+04   0.282E+04       0.986    0.394       49
    41.0       0.189E+04   0.217E+04   0.288E+04       0.984    0.407       50
    40.0       0.188E+04   0.225E+04   0.293E+04       0.983    0.421       51
    39.0       0.188E+04   0.232E+04   0.299E+04       0.981    0.436       52
    38.0       0.188E+04   0.240E+04   0.305E+04       0.979    0.450       53
    37.0       0.187E+04   0.248E+04   0.311E+04       0.977    0.466       54
    36.0       0.187E+04   0.257E+04   0.318E+04       0.974    0.482       55
    35.0       0.186E+04   0.266E+04   0.324E+04       0.971    0.498       56
    34.0       0.185E+04   0.275E+04   0.332E+04       0.967    0.516       57
    33.0       0.185E+04   0.284E+04   0.339E+04       0.963    0.533       58
    32.0       0.184E+04   0.294E+04   0.347E+04       0.959    0.552       59
    31.0       0.183E+04   0.304E+04   0.355E+04       0.953    0.570       60
    30.0       0.182E+04   0.315E+04   0.363E+04       0.947    0.590       61
    29.0       0.180E+04   0.325E+04   0.372E+04       0.941    0.610       62
    28.0       0.179E+04   0.336E+04   0.381E+04       0.933    0.631       63
    27.0       0.177E+04   0.347E+04   0.390E+04       0.924    0.652       64
    26.0       0.175E+04   0.359E+04   0.399E+04       0.913    0.673       65
    25.0       0.173E+04   0.371E+04   0.409E+04       0.901    0.695       66
    24.0       0.170E+04   0.382E+04   0.418E+04       0.888    0.717       67
    23.0       0.167E+04   0.394E+04   0.428E+04       0.873    0.739       68
    22.0       0.164E+04   0.406E+04   0.438E+04       0.856    0.761       69
    21.0       0.160E+04   0.418E+04   0.447E+04       0.836    0.783       70
    20.0       0.156E+04   0.429E+04   0.457E+04       0.815    0.805       71
    19.0       0.152E+04   0.440E+04   0.466E+04       0.791    0.826       72
    18.0       0.147E+04   0.451E+04   0.474E+04       0.765    0.846       73
    17.0       0.141E+04   0.461E+04   0.482E+04       0.736    0.865       74
    16.0       0.135E+04   0.471E+04   0.490E+04       0.705    0.883       75
    15.0       0.129E+04   0.480E+04   0.497E+04       0.671    0.900       76
    14.0       0.122E+04   0.489E+04   0.503E+04       0.635    0.916       77
    13.0       0.115E+04   0.496E+04   0.509E+04       0.598    0.930       78
    12.0       0.107E+04   0.503E+04   0.514E+04       0.558    0.943       79
    11.0        989.       0.509E+04   0.518E+04       0.516    0.954       80
    10.0        907.       0.514E+04   0.522E+04       0.473    0.964       81
    9.00        821.       0.519E+04   0.525E+04       0.429    0.973       82
    8.00        734.       0.522E+04   0.528E+04       0.383    0.980       83
    7.00        645.       0.525E+04   0.529E+04       0.337    0.985       84
    6.00        555.       0.528E+04   0.531E+04       0.290    0.990       85
    5.00        464.       0.530E+04   0.532E+04       0.242    0.994       86
    4.00        372.       0.531E+04   0.533E+04       0.194    0.997       87
    3.00        279.       0.533E+04   0.533E+04       0.146    0.999       88
    2.00        186.       0.533E+04   0.534E+04       0.097    1.000       89
    1.00        93.2       0.534E+04   0.534E+04       0.049    1.002       90
    0.00        0.00       0.535E+04   0.535E+04       0.000    1.002       91
   -1.00       -93.4       0.535E+04   0.535E+04      -0.049    1.003       92
   -2.00       -187.       0.535E+04   0.535E+04      -0.097    1.003       93
   -3.00       -280.       0.535E+04   0.536E+04      -0.146    1.003       94
   -4.00       -374.       0.534E+04   0.536E+04      -0.195    1.002       95
   -5.00       -467.       0.534E+04   0.536E+04      -0.244    1.001       96
   -6.00       -560.       0.532E+04   0.535E+04      -0.292    0.998       97
   -7.00       -651.       0.531E+04   0.535E+04      -0.340    0.995       98
   -8.00       -742.       0.528E+04   0.533E+04      -0.387    0.990       99
   -9.00       -831.       0.525E+04   0.531E+04      -0.434    0.984      100
   -10.0       -918.       0.521E+04   0.529E+04      -0.479    0.977      101
   -11.0      -0.100E+04   0.516E+04   0.526E+04      -0.523    0.968      102
   -12.0      -0.108E+04   0.510E+04   0.522E+04      -0.566    0.957      103
   -13.0      -0.116E+04   0.504E+04   0.517E+04      -0.607    0.945      104
   -14.0      -0.124E+04   0.496E+04   0.511E+04      -0.646    0.931      105
   -15.0      -0.131E+04   0.488E+04   0.505E+04      -0.682    0.915      106
   -16.0      -0.137E+04   0.479E+04   0.498E+04      -0.716    0.898      107
   -17.0      -0.143E+04   0.469E+04   0.490E+04      -0.748    0.879      108
   -18.0      -0.149E+04   0.458E+04   0.482E+04      -0.777    0.859      109
   -19.0      -0.154E+04   0.447E+04   0.473E+04      -0.803    0.839      110
   -20.0      -0.159E+04   0.436E+04   0.464E+04      -0.827    0.817      111
   -21.0      -0.163E+04   0.424E+04   0.454E+04      -0.848    0.794      112
   -22.0      -0.166E+04   0.411E+04   0.444E+04      -0.867    0.772      113
   -23.0      -0.169E+04   0.399E+04   0.434E+04      -0.884    0.749      114
   -24.0      -0.172E+04   0.387E+04   0.424E+04      -0.899    0.726      115
   -25.0      -0.175E+04   0.375E+04   0.413E+04      -0.912    0.703      116
   -26.0      -0.177E+04   0.363E+04   0.404E+04      -0.923    0.680      117
   -27.0      -0.179E+04   0.351E+04   0.394E+04      -0.932    0.658      118
   -28.0      -0.180E+04   0.339E+04   0.384E+04      -0.941    0.636      119
   -29.0      -0.182E+04   0.328E+04   0.375E+04      -0.948    0.615      120
   -30.0      -0.183E+04   0.317E+04   0.366E+04      -0.955    0.594      121
   -31.0      -0.184E+04   0.306E+04   0.357E+04      -0.960    0.574      122
   -32.0      -0.185E+04   0.296E+04   0.349E+04      -0.965    0.555      123
   -33.0      -0.186E+04   0.286E+04   0.341E+04      -0.969    0.536      124
   -34.0      -0.186E+04   0.276E+04   0.333E+04      -0.972    0.518      125
   -35.0      -0.187E+04   0.267E+04   0.326E+04      -0.976    0.501      126
   -36.0      -0.188E+04   0.258E+04   0.319E+04      -0.978    0.484      127
   -37.0      -0.188E+04   0.249E+04   0.312E+04      -0.981    0.468      128
   -38.0      -0.188E+04   0.241E+04   0.306E+04      -0.983    0.452      129
   -39.0      -0.189E+04   0.233E+04   0.300E+04      -0.984    0.437      130
   -40.0      -0.189E+04   0.225E+04   0.294E+04      -0.986    0.422      131
   -41.0      -0.189E+04   0.218E+04   0.288E+04      -0.987    0.408      132
   -42.0      -0.189E+04   0.210E+04   0.283E+04      -0.989    0.395      133
   -43.0      -0.190E+04   0.203E+04   0.278E+04      -0.990    0.381      134
   -44.0      -0.190E+04   0.197E+04   0.273E+04      -0.991    0.369      135
   -45.0      -0.190E+04   0.190E+04   0.269E+04      -0.991    0.356      136
   -46.0      -0.190E+04   0.184E+04   0.264E+04      -0.992    0.344      137
   -47.0      -0.190E+04   0.177E+04   0.260E+04      -0.993    0.333      138
   -48.0      -0.190E+04   0.171E+04   0.256E+04      -0.993    0.322      139
   -49.0      -0.191E+04   0.166E+04   0.252E+04      -0.994    0.311      140
   -50.0      -0.191E+04   0.160E+04   0.249E+04      -0.994    0.300      141
   -51.0      -0.191E+04   0.154E+04   0.245E+04      -0.995    0.290      142
   -52.0      -0.191E+04   0.149E+04   0.242E+04      -0.995    0.280      143
   -53.0      -0.191E+04   0.144E+04   0.239E+04      -0.996    0.270      144
   -54.0      -0.191E+04   0.139E+04   0.236E+04      -0.996    0.260      145
   -55.0      -0.191E+04   0.134E+04   0.233E+04      -0.996    0.251      146
   -56.0      -0.191E+04   0.129E+04   0.230E+04      -0.996    0.242      147
   -57.0      -0.191E+04   0.124E+04   0.228E+04      -0.997    0.233      148
   -58.0      -0.191E+04   0.119E+04   0.225E+04      -0.997    0.224      149
   -59.0      -0.191E+04   0.115E+04   0.223E+04      -0.997    0.215      150
   -60.0      -0.191E+04   0.110E+04   0.221E+04      -0.997    0.207      151
   -61.0      -0.191E+04   0.106E+04   0.219E+04      -0.997    0.199      152
   -62.0      -0.191E+04   0.102E+04   0.217E+04      -0.997    0.191      153
   -63.0      -0.191E+04    974.       0.215E+04      -0.997    0.183      154
   -64.0      -0.191E+04    933.       0.213E+04      -0.998    0.175      155
   -65.0      -0.191E+04    892.       0.211E+04      -0.998    0.167      156
   -66.0      -0.191E+04    852.       0.209E+04      -0.998    0.160      157
   -67.0      -0.191E+04    812.       0.208E+04      -0.998    0.152      158
   -68.0      -0.191E+04    773.       0.206E+04      -0.998    0.145      159
   -69.0      -0.191E+04    734.       0.205E+04      -0.998    0.138      160
   -70.0      -0.191E+04    697.       0.204E+04      -0.998    0.131      161
   -71.0      -0.191E+04    659.       0.202E+04      -0.998    0.124      162
   -72.0      -0.191E+04    622.       0.201E+04      -0.998    0.117      163
   -73.0      -0.191E+04    585.       0.200E+04      -0.998    0.110      164
   -74.0      -0.191E+04    549.       0.199E+04      -0.998    0.103      165
   -75.0      -0.191E+04    513.       0.198E+04      -0.999    0.096      166
   -76.0      -0.191E+04    477.       0.197E+04      -0.999    0.089      167
   -77.0      -0.191E+04    442.       0.196E+04      -0.999    0.083      168
   -78.0      -0.191E+04    407.       0.196E+04      -0.999    0.076      169
   -79.0      -0.191E+04    372.       0.195E+04      -0.999    0.070      170
   -80.0      -0.191E+04    338.       0.194E+04      -0.999    0.063      171
   -81.0      -0.191E+04    303.       0.194E+04      -0.999    0.057      172
   -82.0      -0.191E+04    269.       0.193E+04      -0.999    0.050      173
   -83.0      -0.191E+04    235.       0.193E+04      -0.999    0.044      174
   -84.0      -0.191E+04    201.       0.192E+04      -0.999    0.038      175
   -85.0      -0.191E+04    167.       0.192E+04      -0.999    0.031      176
   -86.0      -0.191E+04    134.       0.192E+04      -0.999    0.025      177
   -87.0      -0.191E+04    100.       0.192E+04      -0.999    0.019      178
   -88.0      -0.191E+04    66.9       0.192E+04      -0.999    0.013      179
   -89.0      -0.191E+04    33.4       0.191E+04      -0.999    0.006      180
   -90.0      -0.191E+04   0.117E-12   0.191E+04      -0.999    0.000      181
------------------------------------------------------------------------------
 theta*     Vlug_theta*  Hlug_theta*  T_theta*   Vlug_theta*  Hlug_theta*  row
  [deg]        [kN]         [kN]        [kN]      / Vmax [-]   / Hmax [-]  [-]
------------------------------------------------------------------------------
VHlug_resist_sub: END --- >

solve_MODE22_sub: END --- >


caisson_vhm: input   file: "JOB.I01"
caisson_vhm: output  file: "JOB.O01"
caisson_vhm: normal program end
