
 p r o g r a m  C A I S S O N _ V H M  w32 version 00.12_b04 
 ------------------------------------  at 17:29:24 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
   0.62   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]:    5322.001
   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]:    1895.488
   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]:    5322.001
   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    5322.001  -53220.009
   Vstar,Hstar,Mstar                     [-]:      -0.289      10.961      -7.307
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.961      -7.307      -0.289
   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)                  [-]:      -0.991
 > f_VHM_fun                             [-]: -0.3012878E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    5327.457
   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]:    1895.488
   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]:     925.103
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5246.521
   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]:     377.071    5246.521  -54546.694
   Vstar,Hstar,Mstar                     [-]:       0.199      10.805      -7.489
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.805      -7.489       0.199
   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                             [-]: -0.5976551E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    5079.212
   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]:    1895.488
   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]:    1737.193
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4772.898
   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]:    1189.161    4772.898  -51637.666
   Vstar,Hstar,Mstar                     [-]:       0.627       9.830      -7.090
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.830      -7.090       0.627
   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           [-]:       0.837
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.055
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.892
 > f_VHM_fun                             [-]:  0.3451062E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    4380.193
   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]:    1895.488
   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]:    2190.096
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3793.358
   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]:    1642.064    3793.358  -42861.300
   Vstar,Hstar,Mstar                     [-]:       0.866       7.812      -5.885
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.812      -5.885       0.866
   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           [-]:       0.544
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.096
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.640
 > f_VHM_fun                             [-]:  0.5612775E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    3659.615
   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]:    1895.488
   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]:    2352.355
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2803.428
   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]:    1804.323    2803.428  -33327.079
   Vstar,Hstar,Mstar                     [-]:       0.952       5.774      -4.576
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.774      -4.576       0.952
   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           [-]:       0.308
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.116
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.424
 > f_VHM_fun                             [-]:  0.3028985E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    3139.874
   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]:    1895.488
   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]:    2405.283
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2018.272
   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]:    1857.251    2018.272  -25594.606
   Vstar,Hstar,Mstar                     [-]:       0.980       4.157      -3.514
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  4.157      -3.514       0.980
   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           [-]:       0.167
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.126
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.292
 > f_VHM_fun                             [-]:  0.4272810E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00043
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    2799.467
   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]:    1895.488
   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]:    2424.409
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1399.733
   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]:    1876.377    1399.733  -19452.256
   Vstar,Hstar,Mstar                     [-]:       0.990       2.883      -2.671
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.883      -2.671       0.990
   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           [-]:       0.086
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.131
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.216
 > f_VHM_fun                             [-]:  0.9364785E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    2587.211
   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]:    1895.488
   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]:    2431.183
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     884.878
   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]:    1883.151     884.878  -14318.944
   Vstar,Hstar,Mstar                     [-]:       0.993       1.822      -1.966
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.822      -1.966       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           [-]:       0.039
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.134
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.178
 > f_VHM_fun                             [-]: -0.5142586E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00514
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    2472.915
   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]:    1895.488
   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]:    2435.346
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     429.417
   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]:    1887.314     429.417   -9773.700
   Vstar,Hstar,Mstar                     [-]:       0.996       0.884      -1.342
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.884      -1.342       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           [-]:       0.137
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.148
 > f_VHM_fun                             [-]:  0.8474525E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00085
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    2436.280
   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]:    1895.488
   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]:    2436.280
   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]:    1888.248       0.000   -5481.629
   Vstar,Hstar,Mstar                     [-]:       0.996       0.000      -0.753
   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      -0.753       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           [-]:       0.139
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.141
 > f_VHM_fun                             [-]: -0.7068266E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00071
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:      945.76570
   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]:     1895.48805
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1756.64692
   Qleaking   = Fo                      [kN]:      945.76570
 > Vmax_fun                             [kN]:     1895.48805
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]:    6020.621
   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]:    2059.270
   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]:    6020.621
   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    6020.621  -63216.520
   Vstar,Hstar,Mstar                     [-]:      -0.282      11.082      -7.273
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 11.082      -7.273      -0.282
   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                             [-]: -0.2975378E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    6078.081
   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]:    2059.270
   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]:    1055.448
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5985.742
   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]:     474.429    5985.742  -65225.043
   Vstar,Hstar,Mstar                     [-]:       0.230      11.018      -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                 11.018      -7.504       0.230
   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                             [-]: -0.6832089E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    5764.224
   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]:    2059.270
   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]:    1971.481
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5416.598
   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]:    1390.462    5416.598  -61310.114
   Vstar,Hstar,Mstar                     [-]:       0.675       9.971      -7.054
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.971      -7.054       0.675
   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           [-]:       0.834
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.028
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.862
 > f_VHM_fun                             [-]:  0.5323335E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    4869.039
   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]:    2059.270
   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]:    2434.520
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4216.712
   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]:    1853.501    4216.712  -49753.143
   Vstar,Hstar,Mstar                     [-]:       0.900       7.762      -5.724
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.762      -5.724       0.900
   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           [-]:       0.519
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.060
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.579
 > f_VHM_fun                             [-]: -0.9120868E-04
f_VHM_fun : END --- >

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


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

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    4007.332
   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]:    2059.270
   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]:    2575.863
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3069.794
   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]:    1994.844    3069.794  -38028.534
   Vstar,Hstar,Mstar                     [-]:       0.969       5.651      -4.375
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.651      -4.375       0.969
   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           [-]:       0.284
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.079
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.363
 > f_VHM_fun                             [-]:  0.3262347E-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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    3414.848
   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]:    2059.270
   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]:    2615.926
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2195.022
   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]:    2034.907    2195.022  -28933.566
   Vstar,Hstar,Mstar                     [-]:       0.988       4.040      -3.329
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  4.040      -3.329       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           [-]:       0.152
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.090
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.241
 > f_VHM_fun                             [-]:  0.2439731E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00024
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    3035.463
   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]:    2059.270
   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]:    2628.788
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1517.732
   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]:    2047.769    1517.732  -21850.956
   Vstar,Hstar,Mstar                     [-]:       0.994       2.794      -2.514
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.794      -2.514       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           [-]:       0.077
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.097
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.175
 > f_VHM_fun                             [-]: -0.6357385E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00064
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    2802.589
   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]:    2059.270
   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]:    2633.572
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     958.542
   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]:    2052.553     958.542  -15990.226
   Vstar,Hstar,Mstar                     [-]:       0.997       1.764      -1.840
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.764      -1.840       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           [-]:       0.103
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.139
 > f_VHM_fun                             [-]: -0.1423891E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00142
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    2675.434
   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]:    2059.270
   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]:    2634.788
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     464.584
   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]:    2053.769     464.584  -10806.407
   Vstar,Hstar,Mstar                     [-]:       0.997       0.855      -1.243
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.855      -1.243       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           [-]:       0.108
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.128
 > f_VHM_fun                             [-]: -0.8533788E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00853
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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]:    2636.135
   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]:    2059.270
   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]:    2636.135
   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]:    2055.116       0.000   -5931.303
   Vstar,Hstar,Mstar                     [-]:       0.998       0.000      -0.682
   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      -0.682       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           [-]:       0.113
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.113
 > f_VHM_fun                             [-]:  0.7401726E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00074
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                              [-]:     0.62000
 > alpha_Fo_twist                        [-]:     0.62000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.62
   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]:     1058.15308
   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]:     2059.26971
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1965.39305
   Qleaking   = Fo                      [kN]:     1058.15308
 > Vmax_fun                             [kN]:     2059.26971
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      1895.5      5332.3      1456.4       548.0         7.2
    1  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    2  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    2  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    3  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    3  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    4  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    4  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    5  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    5  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    6  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    6  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    7  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    7  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    8  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    8  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

    9  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
    9  2   4.50  16.00   3.56      2059.3      6024.5      1635.1       581.0         7.5

   10  1   4.50  15.00   3.33      1895.5      5332.3      1456.4       548.0         7.2
   10  2   4.50  16.00   3.56      2059.3      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   5322.0   548.0       5  -0.301E-05   ! ? missing text
    1  2   4.50  16.00  10.50  0.00   6020.6   581.0       5  -0.298E-05   ! ? missing text

    2  1   4.50  15.00  10.00 10.00   5327.5   548.0       5  -0.598E-05   ! ? missing text
    2  2   4.50  16.00  10.50 10.00   6078.1   581.0       5  -0.683E-05   ! ? missing text

    3  1   4.50  15.00  10.00 20.00   5079.2   548.0       6   0.345E-06   ! ? missing text
    3  2   4.50  16.00  10.50 20.00   5764.2   581.0       6   0.532E-06   ! ? missing text

    4  1   4.50  15.00  10.00 30.00   4380.2   548.0       6   0.561E-06   ! ? missing text
    4  2   4.50  16.00  10.50 30.00   4869.0   581.0       5  -0.912E-04   ! ? missing text

    5  1   4.50  15.00  10.00 40.00   3659.6   548.0       5   0.303E-04   ! ? missing text
    5  2   4.50  16.00  10.50 40.00   4007.3   581.0       4   0.326E-05   ! ? missing text

    6  1   4.50  15.00  10.00 50.00   3139.9   548.0       7   0.427E-03   ! ? missing text
    6  2   4.50  16.00  10.50 50.00   3414.8   581.0       6   0.244E-03   ! ? missing text

    7  1   4.50  15.00  10.00 60.00   2799.5   548.0       8   0.936E-03   ! ? missing text
    7  2   4.50  16.00  10.50 60.00   3035.5   581.0       9  -0.636E-03   ! ? missing text

    8  1   4.50  15.00  10.00 70.00   2587.2   548.0       8  -0.514E-02   ! ? missing text
    8  2   4.50  16.00  10.50 70.00   2802.6   581.0       9  -0.142E-02   ! ? missing text

    9  1   4.50  15.00  10.00 80.00   2472.9   548.0       8   0.847E-03   ! ? missing text
    9  2   4.50  16.00  10.50 80.00   2675.4   581.0      10  -0.853E-02   ! ? missing text

   10  1   4.50  15.00  10.00 90.00   2436.3   548.0       8  -0.707E-03   ! ? missing text
   10  2   4.50  16.00  10.50 90.00   2636.1   581.0       8   0.740E-03   ! ? 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] =    0.190E+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       0.189E+04   0.116E-12   0.189E+04       0.998    0.000        1
    89.0       0.189E+04    33.0       0.189E+04       0.999    0.006        2
    88.0       0.189E+04    66.1       0.189E+04       0.999    0.012        3
    87.0       0.189E+04    99.2       0.190E+04       0.999    0.019        4
    86.0       0.189E+04    132.       0.190E+04       0.999    0.025        5
    85.0       0.189E+04    166.       0.190E+04       0.999    0.031        6
    84.0       0.189E+04    199.       0.190E+04       0.999    0.037        7
    83.0       0.189E+04    232.       0.191E+04       0.999    0.044        8
    82.0       0.189E+04    266.       0.191E+04       0.999    0.050        9
    81.0       0.189E+04    300.       0.192E+04       0.999    0.056       10
    80.0       0.189E+04    334.       0.192E+04       0.999    0.063       11
    79.0       0.189E+04    368.       0.193E+04       0.999    0.069       12
    78.0       0.189E+04    402.       0.193E+04       0.999    0.075       13
    77.0       0.189E+04    437.       0.194E+04       0.998    0.082       14
    76.0       0.189E+04    472.       0.195E+04       0.998    0.088       15
    75.0       0.189E+04    507.       0.196E+04       0.998    0.095       16
    74.0       0.189E+04    543.       0.197E+04       0.998    0.102       17
    73.0       0.189E+04    579.       0.198E+04       0.998    0.108       18
    72.0       0.189E+04    615.       0.199E+04       0.998    0.115       19
    71.0       0.189E+04    651.       0.200E+04       0.998    0.122       20
    70.0       0.189E+04    688.       0.201E+04       0.998    0.129       21
    69.0       0.189E+04    726.       0.202E+04       0.997    0.136       22
    68.0       0.189E+04    764.       0.204E+04       0.998    0.143       23
    67.0       0.189E+04    803.       0.205E+04       0.997    0.151       24
    66.0       0.189E+04    842.       0.207E+04       0.998    0.158       25
    65.0       0.189E+04    882.       0.209E+04       0.997    0.165       26
    64.0       0.189E+04    922.       0.210E+04       0.997    0.173       27
    63.0       0.189E+04    963.       0.212E+04       0.997    0.181       28
    62.0       0.189E+04   0.100E+04   0.214E+04       0.997    0.188       29
    61.0       0.189E+04   0.105E+04   0.216E+04       0.996    0.196       30
    60.0       0.189E+04   0.109E+04   0.218E+04       0.997    0.205       31
    59.0       0.189E+04   0.113E+04   0.220E+04       0.996    0.213       32
    58.0       0.189E+04   0.118E+04   0.223E+04       0.996    0.221       33
    57.0       0.189E+04   0.123E+04   0.225E+04       0.996    0.230       34
    56.0       0.189E+04   0.127E+04   0.228E+04       0.996    0.239       35
    55.0       0.189E+04   0.132E+04   0.230E+04       0.995    0.248       36
    54.0       0.189E+04   0.137E+04   0.233E+04       0.995    0.257       37
    53.0       0.189E+04   0.142E+04   0.236E+04       0.995    0.266       38
    52.0       0.188E+04   0.147E+04   0.239E+04       0.994    0.276       39
    51.0       0.188E+04   0.153E+04   0.242E+04       0.994    0.286       40
    50.0       0.188E+04   0.158E+04   0.246E+04       0.993    0.296       41
    49.0       0.188E+04   0.164E+04   0.249E+04       0.993    0.307       42
    48.0       0.188E+04   0.169E+04   0.253E+04       0.992    0.318       43
    47.0       0.188E+04   0.175E+04   0.257E+04       0.991    0.329       44
    46.0       0.188E+04   0.181E+04   0.261E+04       0.991    0.340       45
    45.0       0.188E+04   0.188E+04   0.265E+04       0.990    0.352       46
    44.0       0.187E+04   0.194E+04   0.270E+04       0.989    0.364       47
    43.0       0.187E+04   0.201E+04   0.275E+04       0.988    0.377       48
    42.0       0.187E+04   0.208E+04   0.279E+04       0.987    0.390       49
    41.0       0.187E+04   0.215E+04   0.285E+04       0.985    0.403       50
    40.0       0.186E+04   0.222E+04   0.290E+04       0.984    0.417       51
    39.0       0.186E+04   0.230E+04   0.296E+04       0.982    0.431       52
    38.0       0.186E+04   0.238E+04   0.302E+04       0.980    0.446       53
    37.0       0.185E+04   0.246E+04   0.308E+04       0.978    0.461       54
    36.0       0.185E+04   0.254E+04   0.314E+04       0.975    0.477       55
    35.0       0.184E+04   0.263E+04   0.321E+04       0.972    0.494       56
    34.0       0.184E+04   0.272E+04   0.328E+04       0.969    0.511       57
    33.0       0.183E+04   0.282E+04   0.336E+04       0.965    0.528       58
    32.0       0.182E+04   0.291E+04   0.344E+04       0.960    0.546       59
    31.0       0.181E+04   0.301E+04   0.352E+04       0.955    0.565       60
    30.0       0.180E+04   0.312E+04   0.360E+04       0.950    0.585       61
    29.0       0.179E+04   0.322E+04   0.369E+04       0.943    0.605       62
    28.0       0.177E+04   0.333E+04   0.378E+04       0.935    0.625       63
    27.0       0.176E+04   0.345E+04   0.387E+04       0.927    0.646       64
    26.0       0.174E+04   0.356E+04   0.396E+04       0.916    0.668       65
    25.0       0.172E+04   0.368E+04   0.406E+04       0.905    0.690       66
    24.0       0.169E+04   0.380E+04   0.416E+04       0.892    0.712       67
    23.0       0.166E+04   0.392E+04   0.425E+04       0.877    0.734       68
    22.0       0.163E+04   0.404E+04   0.435E+04       0.860    0.757       69
    21.0       0.159E+04   0.415E+04   0.445E+04       0.841    0.779       70
    20.0       0.155E+04   0.427E+04   0.454E+04       0.820    0.801       71
    19.0       0.151E+04   0.438E+04   0.464E+04       0.796    0.822       72
    18.0       0.146E+04   0.449E+04   0.472E+04       0.770    0.843       73
    17.0       0.141E+04   0.460E+04   0.481E+04       0.742    0.862       74
    16.0       0.135E+04   0.470E+04   0.489E+04       0.711    0.881       75
    15.0       0.128E+04   0.479E+04   0.496E+04       0.677    0.898       76
    14.0       0.122E+04   0.488E+04   0.502E+04       0.641    0.914       77
    13.0       0.114E+04   0.495E+04   0.508E+04       0.603    0.929       78
    12.0       0.107E+04   0.502E+04   0.513E+04       0.563    0.942       79
    11.0        988.       0.508E+04   0.518E+04       0.521    0.953       80
    10.0        906.       0.514E+04   0.522E+04       0.478    0.964       81
    9.00        821.       0.518E+04   0.525E+04       0.433    0.972       82
    8.00        734.       0.522E+04   0.527E+04       0.387    0.979       83
    7.00        645.       0.525E+04   0.529E+04       0.340    0.985       84
    6.00        555.       0.528E+04   0.531E+04       0.293    0.990       85
    5.00        464.       0.530E+04   0.532E+04       0.245    0.994       86
    4.00        372.       0.531E+04   0.533E+04       0.196    0.997       87
    3.00        279.       0.533E+04   0.533E+04       0.147    0.999       88
    2.00        186.       0.533E+04   0.534E+04       0.098    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      -0.099    1.003       93
   -3.00       -280.       0.535E+04   0.536E+04      -0.148    1.003       94
   -4.00       -374.       0.534E+04   0.536E+04      -0.197    1.002       95
   -5.00       -467.       0.534E+04   0.536E+04      -0.246    1.001       96
   -6.00       -559.       0.532E+04   0.535E+04      -0.295    0.998       97
   -7.00       -651.       0.530E+04   0.534E+04      -0.344    0.995       98
   -8.00       -742.       0.528E+04   0.533E+04      -0.391    0.990       99
   -9.00       -831.       0.525E+04   0.531E+04      -0.438    0.984      100
   -10.0       -918.       0.520E+04   0.529E+04      -0.484    0.976      101
   -11.0      -0.100E+04   0.516E+04   0.525E+04      -0.529    0.967      102
   -12.0      -0.108E+04   0.510E+04   0.521E+04      -0.572    0.956      103
   -13.0      -0.116E+04   0.503E+04   0.516E+04      -0.613    0.943      104
   -14.0      -0.123E+04   0.495E+04   0.510E+04      -0.651    0.929      105
   -15.0      -0.130E+04   0.487E+04   0.504E+04      -0.688    0.913      106
   -16.0      -0.137E+04   0.477E+04   0.497E+04      -0.722    0.895      107
   -17.0      -0.143E+04   0.467E+04   0.489E+04      -0.754    0.876      108
   -18.0      -0.148E+04   0.456E+04   0.480E+04      -0.782    0.856      109
   -19.0      -0.153E+04   0.445E+04   0.471E+04      -0.808    0.835      110
   -20.0      -0.158E+04   0.433E+04   0.461E+04      -0.832    0.813      111
   -21.0      -0.162E+04   0.421E+04   0.451E+04      -0.853    0.790      112
   -22.0      -0.165E+04   0.409E+04   0.441E+04      -0.872    0.767      113
   -23.0      -0.168E+04   0.397E+04   0.431E+04      -0.888    0.744      114
   -24.0      -0.171E+04   0.384E+04   0.421E+04      -0.902    0.720      115
   -25.0      -0.173E+04   0.372E+04   0.410E+04      -0.915    0.697      116
   -26.0      -0.175E+04   0.360E+04   0.400E+04      -0.926    0.675      117
   -27.0      -0.177E+04   0.348E+04   0.390E+04      -0.935    0.652      118
   -28.0      -0.179E+04   0.336E+04   0.381E+04      -0.943    0.631      119
   -29.0      -0.180E+04   0.325E+04   0.372E+04      -0.950    0.609      120
   -30.0      -0.181E+04   0.314E+04   0.363E+04      -0.957    0.589      121
   -31.0      -0.182E+04   0.303E+04   0.354E+04      -0.962    0.569      122
   -32.0      -0.183E+04   0.293E+04   0.346E+04      -0.966    0.550      123
   -33.0      -0.184E+04   0.283E+04   0.338E+04      -0.970    0.531      124
   -34.0      -0.185E+04   0.274E+04   0.330E+04      -0.974    0.513      125
   -35.0      -0.185E+04   0.264E+04   0.323E+04      -0.977    0.496      126
   -36.0      -0.186E+04   0.255E+04   0.316E+04      -0.979    0.479      127
   -37.0      -0.186E+04   0.247E+04   0.309E+04      -0.981    0.463      128
   -38.0      -0.186E+04   0.239E+04   0.303E+04      -0.983    0.447      129
   -39.0      -0.187E+04   0.231E+04   0.297E+04      -0.985    0.432      130
   -40.0      -0.187E+04   0.223E+04   0.291E+04      -0.987    0.418      131
   -41.0      -0.187E+04   0.215E+04   0.285E+04      -0.988    0.404      132
   -42.0      -0.187E+04   0.208E+04   0.280E+04      -0.989    0.390      133
   -43.0      -0.188E+04   0.201E+04   0.275E+04      -0.990    0.377      134
   -44.0      -0.188E+04   0.195E+04   0.270E+04      -0.991    0.365      135
   -45.0      -0.188E+04   0.188E+04   0.266E+04      -0.992    0.353      136
   -46.0      -0.188E+04   0.182E+04   0.261E+04      -0.992    0.341      137
   -47.0      -0.188E+04   0.176E+04   0.257E+04      -0.993    0.329      138
   -48.0      -0.188E+04   0.170E+04   0.253E+04      -0.994    0.318      139
   -49.0      -0.188E+04   0.164E+04   0.250E+04      -0.994    0.307      140
   -50.0      -0.189E+04   0.158E+04   0.246E+04      -0.995    0.297      141
   -51.0      -0.189E+04   0.153E+04   0.243E+04      -0.995    0.286      142
   -52.0      -0.189E+04   0.147E+04   0.239E+04      -0.996    0.276      143
   -53.0      -0.189E+04   0.142E+04   0.236E+04      -0.996    0.267      144
   -54.0      -0.189E+04   0.137E+04   0.233E+04      -0.996    0.257      145
   -55.0      -0.189E+04   0.132E+04   0.231E+04      -0.996    0.248      146
   -56.0      -0.189E+04   0.127E+04   0.228E+04      -0.997    0.239      147
   -57.0      -0.189E+04   0.123E+04   0.225E+04      -0.997    0.230      148
   -58.0      -0.189E+04   0.118E+04   0.223E+04      -0.997    0.221      149
   -59.0      -0.189E+04   0.114E+04   0.221E+04      -0.997    0.213      150
   -60.0      -0.189E+04   0.109E+04   0.218E+04      -0.997    0.205      151
   -61.0      -0.189E+04   0.105E+04   0.216E+04      -0.997    0.197      152
   -62.0      -0.189E+04   0.101E+04   0.214E+04      -0.998    0.189      153
   -63.0      -0.189E+04    964.       0.212E+04      -0.998    0.181      154
   -64.0      -0.189E+04    923.       0.210E+04      -0.998    0.173      155
   -65.0      -0.189E+04    882.       0.209E+04      -0.998    0.165      156
   -66.0      -0.189E+04    842.       0.207E+04      -0.997    0.158      157
   -67.0      -0.189E+04    803.       0.205E+04      -0.998    0.151      158
   -68.0      -0.189E+04    764.       0.204E+04      -0.998    0.143      159
   -69.0      -0.189E+04    726.       0.203E+04      -0.998    0.136      160
   -70.0      -0.189E+04    689.       0.201E+04      -0.998    0.129      161
   -71.0      -0.189E+04    652.       0.200E+04      -0.998    0.122      162
   -72.0      -0.189E+04    615.       0.199E+04      -0.998    0.115      163
   -73.0      -0.189E+04    579.       0.198E+04      -0.998    0.109      164
   -74.0      -0.189E+04    543.       0.197E+04      -0.999    0.102      165
   -75.0      -0.189E+04    507.       0.196E+04      -0.999    0.095      166
   -76.0      -0.189E+04    472.       0.195E+04      -0.999    0.089      167
   -77.0      -0.189E+04    437.       0.194E+04      -0.999    0.082      168
   -78.0      -0.189E+04    402.       0.194E+04      -0.999    0.075      169
   -79.0      -0.189E+04    368.       0.193E+04      -0.999    0.069      170
   -80.0      -0.189E+04    334.       0.192E+04      -0.999    0.063      171
   -81.0      -0.189E+04    300.       0.192E+04      -0.999    0.056      172
   -82.0      -0.189E+04    266.       0.191E+04      -0.999    0.050      173
   -83.0      -0.189E+04    232.       0.191E+04      -0.998    0.044      174
   -84.0      -0.189E+04    199.       0.190E+04      -0.999    0.037      175
   -85.0      -0.189E+04    166.       0.190E+04      -0.999    0.031      176
   -86.0      -0.189E+04    132.       0.190E+04      -0.999    0.025      177
   -87.0      -0.189E+04    99.2       0.190E+04      -0.999    0.019      178
   -88.0      -0.189E+04    66.1       0.189E+04      -0.998    0.012      179
   -89.0      -0.189E+04    33.0       0.189E+04      -0.998    0.006      180
   -90.0      -0.189E+04   0.116E-12   0.189E+04      -0.998    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
