
 p r o g r a m  C A I S S O N _ V H M  w32 version 00.12_b04 
 ------------------------------------  at 16:13:29 on 21-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
    1.00    
 gmdata: END --- >


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


 cfdata: < --- BEGIN
 ncgeom
    2
 cgeom
 CIRCULAR
 nfhxp  wt_D_side  wt_D_top
  0   0.780E-02   0.111E-01
 iro_lug  r_lug_user
  1    0.00    
 D  L  zlug
   4.50  15.00  10.00
   4.50  16.00  10.50
 cfdata: END --- >


 ssidat: < --- BEGIN
 alpha_Fo  alpha_Fi  eta_Fo
   0.63   0.54   1.00
 eta_reb  alpha_d_su  iplug_vmode  vmax_user
   1.00   0.50    2   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]:    6932.693
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    6932.693
   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    6932.693  -69326.935
   Vstar,Hstar,Mstar                     [-]:      -0.237      10.983      -7.322
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.983      -7.322      -0.237
   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           [-]:       0.994
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.001
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.995
 > f_VHM_fun                             [-]: -0.2962535E-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                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6907.175
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    1199.418
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6802.240
   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]:     651.386    6802.240  -70721.091
   Vstar,Hstar,Mstar                     [-]:       0.282      10.776      -7.469
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.776      -7.469       0.282
   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           [-]:       0.981
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.011
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.992
 > f_VHM_fun                             [-]: -0.8859556E-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                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    6388.528
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2185.005
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6003.253
   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]:    1636.973    6003.253  -64948.791
   Vstar,Hstar,Mstar                     [-]:       0.708       9.510      -6.860
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.510      -6.860       0.708
   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           [-]:       0.784
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.051
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.835
 > f_VHM_fun                             [-]:  0.4245409E-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                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5294.093
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2647.046
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4584.819
   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]:    2099.015    4584.819  -51804.044
   Vstar,Hstar,Mstar                     [-]:       0.908       7.263      -5.471
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.263      -5.471       0.908
   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           [-]:       0.471
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.083
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.553
 > f_VHM_fun                             [-]: -0.1391114E-04
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4336.556
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2787.484
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3321.995
   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]:    2239.452    3321.995  -39491.785
   Vstar,Hstar,Mstar                     [-]:       0.969       5.263      -4.171
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.263      -4.171       0.969
   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           [-]:       0.256
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.097
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.353
 > f_VHM_fun                             [-]: -0.7180222E-04
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3694.032
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2829.793
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2374.478
   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]:    2281.761    2374.478  -30111.817
   Vstar,Hstar,Mstar                     [-]:       0.987       3.762      -3.180
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  3.762      -3.180       0.987
   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           [-]:       0.137
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.103
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.240
 > f_VHM_fun                             [-]: -0.1156339E-03
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3284.621
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2844.566
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1642.311
   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]:    2296.534    1642.311  -22823.380
   Vstar,Hstar,Mstar                     [-]:       0.994       2.602      -2.410
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.602      -2.410       0.994
   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           [-]:       0.070
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.106
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.177
 > f_VHM_fun                             [-]: -0.5089809E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00051
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3033.514
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2850.571
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1037.523
   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]:    2302.539    1037.523  -16789.015
   Vstar,Hstar,Mstar                     [-]:       0.996       1.644      -1.773
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.644      -1.773       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           [-]:       0.032
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.109
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.141
 > f_VHM_fun                             [-]: -0.2838833E-03
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2897.139
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2853.125
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     503.083
   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]:    2305.093     503.083  -11450.360
   Vstar,Hstar,Mstar                     [-]:       0.997       0.797      -1.209
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  15.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.797      -1.209       0.997
   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           [-]:       0.010
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.111
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.121
 > f_VHM_fun                             [-]: -0.3371189E-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                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    2854.525
   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]:       9.352
   Vmax                                 [kN]:    2311.404
   Hfac=L   D su_av_L                   [kN]:     631.227
   Mfac=L^2 D su_av_L                  [kNm]:    9468.400
   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]:    2854.525
   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]:    2306.493       0.000   -6422.681
   Vstar,Hstar,Mstar                     [-]:       0.998       0.000      -0.678
   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      -0.678       0.998
   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           [-]:       0.113
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.108
 > f_VHM_fun                             [-]:  0.5211721E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00521
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  15.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.35    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1257.25822
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1054.14557
   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]:    17.3    
   qv_tip = Nc * su_av_tip             [kPa]     155.    
   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]:   0.247E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3726.53630
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2311.40379
   Qleaking   = Fo                      [kN]:     1257.25822
 > Vmax_fun                             [kN]:     2311.40379
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    7843.485
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    7843.485
   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    7843.485  -82356.592
   Vstar,Hstar,Mstar                     [-]:      -0.225      11.106      -7.288
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 11.106      -7.288      -0.225
   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           [-]:       0.987
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.009
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.996
 > f_VHM_fun                             [-]: -0.2946533E-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                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    7877.182
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    1367.858
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    7757.510
   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]:     786.839    7757.510  -84531.538
   Vstar,Hstar,Mstar                     [-]:       0.304      10.984      -7.481
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                 10.984      -7.481       0.304
   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           [-]:       0.988
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.002
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.989
 > f_VHM_fun                             [-]: -0.9653675E-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                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    7271.661
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    2487.054
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6833.126
   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]:    1906.035    6833.126  -77343.693
   Vstar,Hstar,Mstar                     [-]:       0.737       9.675      -6.845
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.675      -6.845       0.737
   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           [-]:       0.785
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.026
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.811
 > f_VHM_fun                             [-]:  0.5307916E-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                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    5956.210
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    2978.105
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    5158.229
   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]:    2397.086    5158.229  -60862.139
   Vstar,Hstar,Mstar                     [-]:       0.927       7.304      -5.386
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.304      -5.386       0.927
   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           [-]:       0.460
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.053
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.513
 > f_VHM_fun                             [-]: -0.6016255E-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                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4838.440
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    3110.089
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3706.460
   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]:    2529.070    3706.460  -45915.533
   Vstar,Hstar,Mstar                     [-]:       0.978       5.248      -4.063
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.248      -4.063       0.978
   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           [-]:       0.245
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.068
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.314
 > f_VHM_fun                             [-]: -0.5065440E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00051
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    4106.652
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    3145.878
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2639.705
   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]:    2564.859    2639.705  -34795.129
   Vstar,Hstar,Mstar                     [-]:       0.992       3.738      -3.079
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  3.738      -3.079       0.992
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      13.371       1.682     -33.965
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      13.371       1.682     -33.965
   aVH , bVH                             [-]:       4.656       3.125
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.130
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.077
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.206
 > f_VHM_fun                             [-]:  0.1790387E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00018
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3645.674
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    3157.246
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1822.837
   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]:    2576.227    1822.837  -26243.593
   Vstar,Hstar,Mstar                     [-]:       0.996       2.581      -2.322
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.581      -2.322       0.996
   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           [-]:       0.066
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.083
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.149
 > f_VHM_fun                             [-]:  0.2613339E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00026
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3364.307
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    3161.415
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1150.661
   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]:    2580.396    1150.661  -19195.123
   Vstar,Hstar,Mstar                     [-]:       0.998       1.629      -1.699
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.629      -1.699       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           [-]:       0.030
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.088
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.118
 > f_VHM_fun                             [-]: -0.6672368E-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                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3211.832
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    3163.037
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     557.729
   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]:    2582.018     557.729  -12972.985
   Vstar,Hstar,Mstar                     [-]:       0.998       0.790      -1.148
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   4.50  16.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.790      -1.148       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           [-]:       0.009
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.092
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.102
 > f_VHM_fun                             [-]: -0.2650147E-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                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:    3163.677
   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]:       9.809
   Vmax                                 [kN]:    2586.073
   Hfac=L   D su_av_L                   [kN]:     706.237
   Mfac=L^2 D su_av_L                  [kNm]:   11299.787
   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]:    3163.677
   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]:    2582.658       0.000   -7118.274
   Vstar,Hstar,Mstar                     [-]:       0.999       0.000      -0.630
   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      -0.630       0.999
   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           [-]:       0.097
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.095
 > f_VHM_fun                             [-]:  0.2715842E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00272
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  16.00   4.50

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

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.63
   alpha_Fi                              [-]:   0.54
   eta_Fo, eta_REB                       [-]:  1.000  1.000
   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]:    9.81    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     1406.66092
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     1179.41196
   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]:    18.2    
   qv_tip = Nc * su_av_tip             [kPa]     164.    
   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]:   0.260E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     4009.56416
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     2586.07288
   Qleaking   = Fo                      [kN]:     1406.66092
 > Vmax_fun                             [kN]:     2586.07288
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                           [-]:  2
 > 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  =  2
 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      2311.4      6931.9      1893.3       548.0         9.4
    1  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    2  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    2  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    3  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    3  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    4  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    4  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    5  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    5  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    6  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    6  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    7  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    7  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    8  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    8  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

    9  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
    9  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8

   10  1   4.50  15.00   3.33      2311.4      6931.9      1893.3       548.0         9.4
   10  2   4.50  16.00   3.56      2586.1      7831.9      2125.6       581.0         9.8
 ----------------------------------------------------------------------------------------
  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   6932.7   548.0       5  -0.296E-05   ! ? missing text
    1  2   4.50  16.00  10.50  0.00   7843.5   581.0       5  -0.295E-05   ! ? missing text

    2  1   4.50  15.00  10.00 10.00   6907.2   548.0       5  -0.886E-05   ! ? missing text
    2  2   4.50  16.00  10.50 10.00   7877.2   581.0       5  -0.965E-05   ! ? missing text

    3  1   4.50  15.00  10.00 20.00   6388.5   548.0       6   0.425E-06   ! ? missing text
    3  2   4.50  16.00  10.50 20.00   7271.7   581.0       6   0.531E-06   ! ? missing text

    4  1   4.50  15.00  10.00 30.00   5294.1   548.0       5  -0.139E-04   ! ? missing text
    4  2   4.50  16.00  10.50 30.00   5956.2   581.0       5  -0.602E-06   ! ? missing text

    5  1   4.50  15.00  10.00 40.00   4336.6   548.0       6  -0.718E-04   ! ? missing text
    5  2   4.50  16.00  10.50 40.00   4838.4   581.0       8  -0.507E-03   ! ? missing text

    6  1   4.50  15.00  10.00 50.00   3694.0   548.0       8  -0.116E-03   ! ? missing text
    6  2   4.50  16.00  10.50 50.00   4106.7   581.0      10   0.179E-03   ! ? missing text

    7  1   4.50  15.00  10.00 60.00   3284.6   548.0       9  -0.509E-03   ! ? missing text
    7  2   4.50  16.00  10.50 60.00   3645.7   581.0       8   0.261E-03   ! ? missing text

    8  1   4.50  15.00  10.00 70.00   3033.5   548.0      12  -0.284E-03   ! ? missing text
    8  2   4.50  16.00  10.50 70.00   3364.3   581.0      24  -0.667E-05   ! ? missing text

    9  1   4.50  15.00  10.00 80.00   2897.1   548.0      24  -0.337E-05   ! ? missing text
    9  2   4.50  16.00  10.50 80.00   3211.8   581.0      24  -0.265E-05   ! ? missing text

   10  1   4.50  15.00  10.00 90.00   2854.5   548.0       8   0.521E-02   ! ? missing text
   10  2   4.50  16.00  10.50 90.00   3163.7   581.0       6   0.272E-02   ! ? missing text
 -----------------------------------------------------------------------
 ilc        D      L    zlug  theta    Tlug     Bw    ( iters    f_VHM )
  icgeom   [m]    [m]   [m]   [deg]    [kN]    [kN]   ( [-]      [-]   )
 -----------------------------------------------------------------------

VHlug_resist_sub: < --- BEGIN
  load case #=    1; caisson geometry #=    1 (#rows results= =  181)
  L         [m] =   15.00
  D         [m] =    4.50
  zlug      [m] =   10.00
  iro_lug   [-] =   1: offset + D/2 (lug on outer face)
  m_fac     [-] =   1.000
  Hmax     [kN] =    0.693E+04
  Vmax     [kN] =    0.231E+04
  theta*        = resistance inclination at lug
  Vlug_theta*, Hlug_theta*
                = corresponding VH UNFACTORED 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       0.231E+04   0.141E-12   0.231E+04       0.999    0.000        1
    89.0       0.231E+04    40.3       0.231E+04       0.999    0.006        2
    88.0       0.231E+04    80.6       0.231E+04       0.999    0.012        3
    87.0       0.231E+04    121.       0.231E+04       0.999    0.017        4
    86.0       0.231E+04    161.       0.231E+04       0.999    0.023        5
    85.0       0.231E+04    202.       0.232E+04       0.999    0.029        6
    84.0       0.231E+04    243.       0.232E+04       0.999    0.035        7
    83.0       0.231E+04    284.       0.233E+04       0.999    0.041        8
    82.0       0.231E+04    324.       0.233E+04       0.999    0.047        9
    81.0       0.231E+04    366.       0.234E+04       0.999    0.053       10
    80.0       0.231E+04    407.       0.234E+04       0.999    0.059       11
    79.0       0.231E+04    449.       0.235E+04       0.999    0.065       12
    78.0       0.231E+04    491.       0.236E+04       0.999    0.071       13
    77.0       0.231E+04    533.       0.237E+04       0.999    0.077       14
    76.0       0.231E+04    576.       0.238E+04       0.999    0.083       15
    75.0       0.231E+04    619.       0.239E+04       0.999    0.089       16
    74.0       0.231E+04    662.       0.240E+04       0.999    0.095       17
    73.0       0.231E+04    706.       0.241E+04       0.999    0.102       18
    72.0       0.231E+04    750.       0.243E+04       0.999    0.108       19
    71.0       0.231E+04    795.       0.244E+04       0.999    0.115       20
    70.0       0.231E+04    840.       0.246E+04       0.999    0.121       21
    69.0       0.231E+04    886.       0.247E+04       0.998    0.128       22
    68.0       0.231E+04    932.       0.249E+04       0.998    0.135       23
    67.0       0.231E+04    979.       0.251E+04       0.998    0.141       24
    66.0       0.231E+04   0.103E+04   0.253E+04       0.998    0.148       25
    65.0       0.231E+04   0.108E+04   0.255E+04       0.998    0.155       26
    64.0       0.231E+04   0.113E+04   0.257E+04       0.998    0.162       27
    63.0       0.231E+04   0.118E+04   0.259E+04       0.998    0.170       28
    62.0       0.231E+04   0.123E+04   0.261E+04       0.998    0.177       29
    61.0       0.231E+04   0.128E+04   0.264E+04       0.997    0.184       30
    60.0       0.231E+04   0.133E+04   0.266E+04       0.997    0.192       31
    59.0       0.231E+04   0.139E+04   0.269E+04       0.997    0.200       32
    58.0       0.230E+04   0.144E+04   0.272E+04       0.997    0.208       33
    57.0       0.230E+04   0.150E+04   0.275E+04       0.997    0.216       34
    56.0       0.230E+04   0.155E+04   0.278E+04       0.997    0.224       35
    55.0       0.230E+04   0.161E+04   0.281E+04       0.997    0.233       36
    54.0       0.230E+04   0.167E+04   0.285E+04       0.996    0.241       37
    53.0       0.230E+04   0.173E+04   0.288E+04       0.996    0.250       38
    52.0       0.230E+04   0.180E+04   0.292E+04       0.996    0.259       39
    51.0       0.230E+04   0.186E+04   0.296E+04       0.995    0.269       40
    50.0       0.230E+04   0.193E+04   0.300E+04       0.995    0.278       41
    49.0       0.230E+04   0.200E+04   0.305E+04       0.995    0.288       42
    48.0       0.230E+04   0.207E+04   0.309E+04       0.994    0.298       43
    47.0       0.230E+04   0.214E+04   0.314E+04       0.994    0.309       44
    46.0       0.230E+04   0.222E+04   0.319E+04       0.993    0.320       45
    45.0       0.229E+04   0.229E+04   0.324E+04       0.992    0.331       46
    44.0       0.229E+04   0.237E+04   0.330E+04       0.991    0.342       47
    43.0       0.229E+04   0.246E+04   0.336E+04       0.991    0.354       48
    42.0       0.229E+04   0.254E+04   0.342E+04       0.990    0.367       49
    41.0       0.229E+04   0.263E+04   0.348E+04       0.989    0.379       50
    40.0       0.228E+04   0.272E+04   0.355E+04       0.988    0.392       51
    39.0       0.228E+04   0.282E+04   0.362E+04       0.986    0.406       52
    38.0       0.228E+04   0.291E+04   0.370E+04       0.985    0.420       53
    37.0       0.227E+04   0.301E+04   0.378E+04       0.983    0.435       54
    36.0       0.227E+04   0.312E+04   0.386E+04       0.981    0.450       55
    35.0       0.226E+04   0.323E+04   0.394E+04       0.979    0.466       56
    34.0       0.226E+04   0.334E+04   0.403E+04       0.976    0.482       57
    33.0       0.225E+04   0.346E+04   0.413E+04       0.973    0.500       58
    32.0       0.224E+04   0.359E+04   0.423E+04       0.969    0.517       59
    31.0       0.223E+04   0.371E+04   0.433E+04       0.965    0.536       60
    30.0       0.222E+04   0.385E+04   0.444E+04       0.961    0.555       61
    29.0       0.221E+04   0.398E+04   0.455E+04       0.955    0.575       62
    28.0       0.219E+04   0.413E+04   0.467E+04       0.949    0.595       63
    27.0       0.218E+04   0.427E+04   0.479E+04       0.942    0.616       64
    26.0       0.216E+04   0.442E+04   0.492E+04       0.933    0.638       65
    25.0       0.213E+04   0.458E+04   0.505E+04       0.924    0.660       66
    24.0       0.211E+04   0.474E+04   0.518E+04       0.912    0.683       67
    23.0       0.208E+04   0.490E+04   0.532E+04       0.899    0.706       68
    22.0       0.204E+04   0.506E+04   0.546E+04       0.884    0.730       69
    21.0       0.200E+04   0.522E+04   0.559E+04       0.867    0.753       70
    20.0       0.196E+04   0.538E+04   0.573E+04       0.848    0.777       71
    19.0       0.191E+04   0.554E+04   0.586E+04       0.826    0.800       72
    18.0       0.185E+04   0.570E+04   0.599E+04       0.801    0.822       73
    17.0       0.179E+04   0.585E+04   0.612E+04       0.774    0.844       74
    16.0       0.172E+04   0.600E+04   0.624E+04       0.744    0.865       75
    15.0       0.164E+04   0.613E+04   0.635E+04       0.711    0.884       76
    14.0       0.156E+04   0.626E+04   0.645E+04       0.675    0.903       77
    13.0       0.147E+04   0.637E+04   0.654E+04       0.636    0.919       78
    12.0       0.138E+04   0.647E+04   0.662E+04       0.595    0.934       79
    11.0       0.128E+04   0.657E+04   0.669E+04       0.552    0.947       80
    10.0       0.117E+04   0.665E+04   0.675E+04       0.507    0.959       81
    9.00       0.106E+04   0.671E+04   0.680E+04       0.460    0.969       82
    8.00        952.       0.677E+04   0.684E+04       0.412    0.977       83
    7.00        837.       0.682E+04   0.687E+04       0.362    0.984       84
    6.00        721.       0.686E+04   0.689E+04       0.312    0.989       85
    5.00        602.       0.689E+04   0.691E+04       0.261    0.993       86
    4.00        483.       0.691E+04   0.692E+04       0.209    0.996       87
    3.00        363.       0.692E+04   0.693E+04       0.157    0.999       88
    2.00        242.       0.693E+04   0.694E+04       0.105    1.000       89
    1.00        121.       0.694E+04   0.694E+04       0.052    1.002       90
    0.00        0.00       0.695E+04   0.695E+04       0.000    1.002       91
   -1.00       -121.       0.695E+04   0.695E+04      -0.053    1.003       92
   -2.00       -243.       0.695E+04   0.696E+04      -0.105    1.003       93
   -3.00       -364.       0.695E+04   0.696E+04      -0.158    1.003       94
   -4.00       -486.       0.695E+04   0.696E+04      -0.210    1.002       95
   -5.00       -607.       0.693E+04   0.696E+04      -0.262    1.000       96
   -6.00       -727.       0.691E+04   0.695E+04      -0.314    0.997       97
   -7.00       -845.       0.688E+04   0.694E+04      -0.366    0.993       98
   -8.00       -962.       0.684E+04   0.691E+04      -0.416    0.987       99
   -9.00      -0.108E+04   0.679E+04   0.688E+04      -0.466    0.980      100
   -10.0      -0.119E+04   0.673E+04   0.684E+04      -0.514    0.971      101
   -11.0      -0.129E+04   0.666E+04   0.678E+04      -0.560    0.960      102
   -12.0      -0.140E+04   0.657E+04   0.671E+04      -0.604    0.947      103
   -13.0      -0.149E+04   0.647E+04   0.664E+04      -0.646    0.933      104
   -14.0      -0.158E+04   0.635E+04   0.654E+04      -0.685    0.916      105
   -15.0      -0.167E+04   0.622E+04   0.644E+04      -0.721    0.898      106
   -16.0      -0.175E+04   0.609E+04   0.633E+04      -0.755    0.878      107
   -17.0      -0.182E+04   0.594E+04   0.621E+04      -0.785    0.857      108
   -18.0      -0.188E+04   0.578E+04   0.608E+04      -0.813    0.834      109
   -19.0      -0.194E+04   0.562E+04   0.594E+04      -0.837    0.811      110
   -20.0      -0.199E+04   0.546E+04   0.581E+04      -0.859    0.787      111
   -21.0      -0.203E+04   0.529E+04   0.566E+04      -0.878    0.763      112
   -22.0      -0.207E+04   0.512E+04   0.552E+04      -0.895    0.738      113
   -23.0      -0.210E+04   0.495E+04   0.538E+04      -0.909    0.714      114
   -24.0      -0.213E+04   0.478E+04   0.524E+04      -0.921    0.690      115
   -25.0      -0.215E+04   0.462E+04   0.510E+04      -0.932    0.666      116
   -26.0      -0.218E+04   0.446E+04   0.496E+04      -0.941    0.643      117
   -27.0      -0.219E+04   0.430E+04   0.483E+04      -0.949    0.621      118
   -28.0      -0.221E+04   0.415E+04   0.470E+04      -0.956    0.599      119
   -29.0      -0.222E+04   0.401E+04   0.458E+04      -0.961    0.578      120
   -30.0      -0.223E+04   0.387E+04   0.447E+04      -0.966    0.558      121
   -31.0      -0.224E+04   0.373E+04   0.436E+04      -0.970    0.539      122
   -32.0      -0.225E+04   0.360E+04   0.425E+04      -0.974    0.520      123
   -33.0      -0.226E+04   0.348E+04   0.415E+04      -0.977    0.502      124
   -34.0      -0.226E+04   0.336E+04   0.405E+04      -0.980    0.484      125
   -35.0      -0.227E+04   0.324E+04   0.396E+04      -0.982    0.468      126
   -36.0      -0.227E+04   0.313E+04   0.387E+04      -0.984    0.452      127
   -37.0      -0.228E+04   0.302E+04   0.379E+04      -0.986    0.436      128
   -38.0      -0.228E+04   0.292E+04   0.371E+04      -0.987    0.421      129
   -39.0      -0.229E+04   0.282E+04   0.363E+04      -0.989    0.407      130
   -40.0      -0.229E+04   0.273E+04   0.356E+04      -0.990    0.393      131
   -41.0      -0.229E+04   0.264E+04   0.349E+04      -0.991    0.380      132
   -42.0      -0.229E+04   0.255E+04   0.343E+04      -0.992    0.367      133
   -43.0      -0.229E+04   0.246E+04   0.336E+04      -0.992    0.355      134
   -44.0      -0.230E+04   0.238E+04   0.330E+04      -0.993    0.343      135
   -45.0      -0.230E+04   0.230E+04   0.325E+04      -0.994    0.331      136
   -46.0      -0.230E+04   0.222E+04   0.320E+04      -0.994    0.320      137
   -47.0      -0.230E+04   0.214E+04   0.314E+04      -0.995    0.309      138
   -48.0      -0.230E+04   0.207E+04   0.310E+04      -0.995    0.299      139
   -49.0      -0.230E+04   0.200E+04   0.305E+04      -0.996    0.289      140
   -50.0      -0.230E+04   0.193E+04   0.301E+04      -0.996    0.279      141
   -51.0      -0.230E+04   0.186E+04   0.296E+04      -0.996    0.269      142
   -52.0      -0.230E+04   0.180E+04   0.292E+04      -0.997    0.260      143
   -53.0      -0.230E+04   0.174E+04   0.289E+04      -0.997    0.250      144
   -54.0      -0.230E+04   0.167E+04   0.285E+04      -0.997    0.241      145
   -55.0      -0.231E+04   0.161E+04   0.281E+04      -0.997    0.233      146
   -56.0      -0.230E+04   0.155E+04   0.278E+04      -0.997    0.224      147
   -57.0      -0.231E+04   0.150E+04   0.275E+04      -0.997    0.216      148
   -58.0      -0.231E+04   0.144E+04   0.272E+04      -0.998    0.208      149
   -59.0      -0.231E+04   0.139E+04   0.269E+04      -0.998    0.200      150
   -60.0      -0.231E+04   0.133E+04   0.266E+04      -0.997    0.192      151
   -61.0      -0.231E+04   0.128E+04   0.264E+04      -0.998    0.184      152
   -62.0      -0.231E+04   0.123E+04   0.261E+04      -0.998    0.177      153
   -63.0      -0.231E+04   0.118E+04   0.259E+04      -0.998    0.170      154
   -64.0      -0.231E+04   0.113E+04   0.257E+04      -0.998    0.162      155
   -65.0      -0.231E+04   0.108E+04   0.255E+04      -0.998    0.155      156
   -66.0      -0.231E+04   0.103E+04   0.253E+04      -0.999    0.148      157
   -67.0      -0.231E+04    980.       0.251E+04      -0.999    0.141      158
   -68.0      -0.231E+04    933.       0.249E+04      -0.999    0.135      159
   -69.0      -0.231E+04    886.       0.247E+04      -0.999    0.128      160
   -70.0      -0.231E+04    840.       0.246E+04      -0.999    0.121      161
   -71.0      -0.231E+04    795.       0.244E+04      -0.999    0.115      162
   -72.0      -0.231E+04    750.       0.243E+04      -0.999    0.108      163
   -73.0      -0.231E+04    706.       0.241E+04      -0.999    0.102      164
   -74.0      -0.231E+04    662.       0.240E+04      -0.999    0.095      165
   -75.0      -0.231E+04    619.       0.239E+04      -0.999    0.089      166
   -76.0      -0.231E+04    576.       0.238E+04      -0.999    0.083      167
   -77.0      -0.231E+04    533.       0.237E+04      -0.999    0.077      168
   -78.0      -0.231E+04    491.       0.236E+04      -0.999    0.071      169
   -79.0      -0.231E+04    449.       0.235E+04      -0.999    0.065      170
   -80.0      -0.231E+04    407.       0.235E+04      -0.999    0.059      171
   -81.0      -0.231E+04    366.       0.234E+04      -0.999    0.053      172
   -82.0      -0.231E+04    324.       0.233E+04      -0.999    0.047      173
   -83.0      -0.231E+04    283.       0.233E+04      -0.999    0.041      174
   -84.0      -0.231E+04    243.       0.232E+04      -0.999    0.035      175
   -85.0      -0.231E+04    202.       0.232E+04      -0.999    0.029      176
   -86.0      -0.231E+04    161.       0.231E+04      -0.999    0.023      177
   -87.0      -0.231E+04    121.       0.231E+04      -0.999    0.017      178
   -88.0      -0.231E+04    80.6       0.231E+04      -0.999    0.012      179
   -89.0      -0.231E+04    40.3       0.231E+04      -0.999    0.006      180
   -90.0      -0.231E+04   0.141E-12   0.231E+04      -0.999    0.000      181
------------------------------------------------------------------------------
 theta*     Vlug_theta*  Hlug_theta*  T_theta*   Vlug_theta*  Hlug_theta*  row
  [deg]        [kN]         [kN]        [kN]      / Vmax [-]   / Hmax [-]  [-]
------------------------------------------------------------------------------
VHlug_resist_sub: END --- >

solve_MODE22_sub: END --- >


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