
 p r o g r a m  C A I S S O N _ V H M  w32 version 00.12_b04 
 ------------------------------------  at 15:36:12 on 22-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
    2
 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  16.00  10.50
 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]:    6021.516
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500       0.000
   zlug_cL                               [m]:      10.500
   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]:    6021.516
   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    6021.516  -63225.919
   Vstar,Hstar,Mstar                     [-]:      -0.279      11.084      -7.274
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 11.084      -7.274      -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           [-]:       0.983
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.009
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.2983886E-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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6078.550
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      10.000
   zlug_cL                               [m]:      10.897
   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]:    1055.529
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5986.203
   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]:     474.510    5986.203  -65230.077
   Vstar,Hstar,Mstar                     [-]:       0.228      11.019      -7.504
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 11.019      -7.504       0.228
   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           [-]:       0.994
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.002
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.996
 > f_VHM_fun                             [-]: -0.6639700E-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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5777.337
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      20.000
   zlug_cL                               [m]:      11.319
   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]:    1975.966
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5428.921
   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]:    1394.947    5428.921  -61449.594
   Vstar,Hstar,Mstar                     [-]:       0.670       9.993      -7.070
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.993      -7.070       0.670
   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           [-]:       0.838
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.028
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.865
 > f_VHM_fun                             [-]:  0.4905563E-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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4898.609
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      30.000
   zlug_cL                               [m]:      11.799
   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]:    2449.304
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4242.320
   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]:    1868.285    4242.320  -50055.289
   Vstar,Hstar,Mstar                     [-]:       0.897       7.809      -5.759
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.809      -5.759       0.897
   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           [-]:       0.526
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.060
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.586
 > f_VHM_fun                             [-]: -0.1061011E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00011
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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4039.353
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      40.000
   zlug_cL                               [m]:      12.388
   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]:    2596.446
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3094.324
   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]:    2015.427    3094.324  -38332.405
   Vstar,Hstar,Mstar                     [-]:       0.967       5.696      -4.410
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.696      -4.410       0.967
   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           [-]:       0.289
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.080
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.369
 > f_VHM_fun                             [-]: -0.2873483E-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]:  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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3444.276
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      50.000
   zlug_cL                               [m]:      13.181
   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]:    2638.468
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2213.938
   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]:    2057.449    2213.938  -29182.899
   Vstar,Hstar,Mstar                     [-]:       0.988       4.075      -3.357
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  4.075      -3.357       0.988
   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           [-]:       0.155
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.091
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.246
 > f_VHM_fun                             [-]:  0.4297277E-04
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00004
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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3062.277
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      60.000
   zlug_cL                               [m]:      14.397
   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]:    2652.009
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1531.138
   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]:    2070.990    1531.138  -22043.972
   Vstar,Hstar,Mstar                     [-]:       0.994       2.818      -2.536
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.818      -2.536       0.994
   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           [-]:       0.079
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.099
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.179
 > f_VHM_fun                             [-]: -0.9610470E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00096
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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2828.303
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      70.000
   zlug_cL                               [m]:      16.682
   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]:    2657.735
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     967.337
   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]:    2076.716     967.337  -16136.939
   Vstar,Hstar,Mstar                     [-]:       0.997       1.781      -1.856
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.781      -1.856       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           [-]:       0.035
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.105
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.136
 > f_VHM_fun                             [-]:  0.4212182E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00421
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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2699.178
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      80.000
   zlug_cL                               [m]:      23.260
   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]:    2658.172
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     468.707
   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]:    2077.153     468.707  -10902.314
   Vstar,Hstar,Mstar                     [-]:       0.997       0.863      -1.254
   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      -1.254       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           [-]:       0.110
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.132
 > f_VHM_fun                             [-]: -0.1069925E-01
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.01070
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 #=    2

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2659.153
   L , D                                 [m]:      16.000       4.500
   zlug , theta_lug_star           [m] [deg]:      10.500      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 --- >



 -----------------------------------------------
 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  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    2  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    2  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    3  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    3  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    4  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    4  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    5  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    5  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    6  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    6  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    7  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    7  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    8  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    8  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

    9  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
    9  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5

   10  1   4.50  15.00   3.33      1916.8      5332.3      1456.4       548.0         7.2
   10  2   4.50  16.00   3.56      2083.2      6024.5      1635.1       581.0         7.5
 ----------------------------------------------------------------------------------------
  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  16.00  10.50  0.00   6021.5   581.0       5  -0.298E-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  16.00  10.50 10.00   6078.6   581.0       5  -0.664E-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  16.00  10.50 20.00   5777.3   581.0       6   0.491E-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  16.00  10.50 30.00   4898.6   581.0       5  -0.106E-03   ! ? 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  16.00  10.50 40.00   4039.4   581.0       4  -0.287E-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  16.00  10.50 50.00   3444.3   581.0       6   0.430E-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  16.00  10.50 60.00   3062.3   581.0       9  -0.961E-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  16.00  10.50 70.00   2828.3   581.0       8   0.421E-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  16.00  10.50 80.00   2699.2   581.0      10  -0.107E-01   ! ? 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  16.00  10.50 90.00   2659.2   581.0      10  -0.634E-02   ! ? 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
