
 p r o g r a m  C A I S S O N _ V H M  w32 version 00.12_b04 
 ------------------------------------  at 15:53:07 on 09-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: "EX6_MODE22_BC1.O1B.PDF"
       : program name    : "CAISSON_VHM"

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

 pidata: END --- >


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


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


 cfdata: < --- BEGIN
 ncgeom
    1
 cgeom
 CIRCULAR
 nfhxp  wt_D_side  wt_D_top
  0   0.655E-02   0.655E-02
 iro_lug  r_lug_user
  1    3.00    
 D  L  zlug
   6.00  12.00   9.00
 cfdata: END --- >


 ssidat: < --- BEGIN
 alpha_Fo  alpha_Fi  eta_Fo
   0.67   0.67   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
    2    1.00        1.00        0.00        665.    
 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. chndat: user-supplied EXTRA buoyant weight, DELTA_BW_USER <= 0 kN.
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]:    4026.565
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000       0.000
   zlug_cL                               [m]:       9.000
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    4026.565
   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]:    -666.141    4026.565  -36239.084
   Vstar,Hstar,Mstar                     [-]:      -0.360       9.101      -6.826
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.101      -6.826      -0.360
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.876
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.109
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.985
 > f_VHM_fun                             [-]: -0.3188659E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    3752.604
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      10.000
   zlug_cL                               [m]:       9.529
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:     651.633
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3695.594
   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]:     -14.508    3695.594  -35215.240
   Vstar,Hstar,Mstar                     [-]:      -0.008       8.353      -6.633
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  8.353      -6.633      -0.008
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.767
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.233
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -1.000
 > f_VHM_fun                             [-]: -0.3061823E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    3501.674
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      20.000
   zlug_cL                               [m]:      10.092
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1197.643
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3290.498
   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]:     531.502    3290.498  -33207.409
   Vstar,Hstar,Mstar                     [-]:       0.287       7.437      -6.255
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  7.437      -6.255       0.287
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.634
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.360
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.993
 > f_VHM_fun                             [-]: -0.1042697E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    3247.767
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      30.000
   zlug_cL                               [m]:      10.732
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1623.883
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2812.648
   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]:     957.742    2812.648  -30185.486
   Vstar,Hstar,Mstar                     [-]:       0.518       6.357      -5.686
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  6.357      -5.686       0.518
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.484
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.460
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.944
 > f_VHM_fun                             [-]: -0.1524137E-04
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  2
 < L,D                                   [m]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    2983.319
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      40.000
   zlug_cL                               [m]:      11.517
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    1917.640
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    2285.355
   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]:    1251.499    2285.355  -26321.114
   Vstar,Hstar,Mstar                     [-]:       0.676       5.165      -4.958
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.165      -4.958       0.676
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.338
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.512
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.850
 > f_VHM_fun                             [-]: -0.7787767E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    2748.077
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      50.000
   zlug_cL                               [m]:      12.575
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2105.149
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1766.430
   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]:    1439.008    1766.430  -22213.319
   Vstar,Hstar,Mstar                     [-]:       0.778       3.993      -4.184
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  3.993      -4.184       0.778
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.217
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.525
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.742
 > f_VHM_fun                             [-]: -0.6578427E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    2567.558
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      60.000
   zlug_cL                               [m]:      14.196
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2223.571
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1283.779
   l_facT, l_fac_BW                      [-]:       1.000       1.000
   Vload=Vlug*l_facT  - Bw*l_fac_Bw
         Hload=Hlug*l_facT
               Mload=-Hload*zlug_cL
   Vstar=Vload/Vmax
         Hstar=Hload/Hfac
               Mstar=Mload/Mfac
   Vload,Hload,Mload         [kN] [kN] [kNm]:    1557.429    1283.779  -18224.723
   Vstar,Hstar,Mstar                     [-]:       0.842       2.902      -3.433
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  2.902      -3.433       0.842
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.127
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.515
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.642
 > f_VHM_fun                             [-]: -0.5957707E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    2447.685
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      70.000
   zlug_cL                               [m]:      17.242
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2300.071
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     837.157
   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]:    1633.930     837.157  -14434.630
   Vstar,Hstar,Mstar                     [-]:       0.883       1.892      -2.719
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.892      -2.719       0.883
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.065
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.493
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.558
 > f_VHM_fun                             [-]:  0.9017086E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    2387.085
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      80.000
   zlug_cL                               [m]:      26.014
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2350.820
   Hlug=Tlug*cos(theta_lug_star)        [kN]:     414.513
   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]:    1684.679     414.513  -10783.078
   Vstar,Hstar,Mstar                     [-]:       0.910       0.937      -2.031
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.937      -2.031       0.910
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.025
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.464
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.489
 > f_VHM_fun                             [-]: -0.8227176E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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]:    2384.863
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       9.000      90.000
   zlug_cL                               [m]:************
   Bw , Bw_plug                         [kN]:     666.141       0.000
   su_av_L                             [kPa]:       6.145
   Vmax                                 [kN]:    1850.308
   Hfac=L   D su_av_L                   [kN]:     442.429
   Mfac=L^2 D su_av_L                  [kNm]:    5309.146
   aMH , bMH                             [-]:      12.141       1.700
   phiMH , phiMH                 [rad] [deg]:      -0.594     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2384.863
   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]:    1718.722       0.000   -7154.589
   Vstar,Hstar,Mstar                     [-]:       0.929       0.000      -1.348
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  0.000      -1.348       0.929
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.141       1.700     -34.042
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.141       1.700     -34.042
   aVH , bVH                             [-]:       3.533       3.546
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.004
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.432
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.435
 > f_VHM_fun                             [-]: -0.1159688E-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]:  12.00   6.00

alpha_Fo_twist: < --- BEGIN
 < psi_twist                           [deg]:   0.00
 < alpha_Fo                              [-]:     0.67000
 > alpha_Fo_twist                        [-]:     0.67000
alpha_Fo_twist: END --- >

   wt_D_side                             [-]:   0.01
   alpha_Fo                              [-]:   0.67
   alpha_Fi                              [-]:   0.67
   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]:   5.92
   su_av_L   = av 0    to L            [kPa]:    6.14    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:      931.25384
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:      919.05441
   Fxp=         2*Di*L*alpha_Fi*su_av_L*nfhxp
                                        [kN]:    0.00    
   L_D = L / D                           [-]:    2.00    
   Nc = min( 6*(1+0.2*L_D) , 9)          [-]:    8.40    
   su_av_tip = av L to L+alpha_d_su*D  [kPa]:    11.4    
   qv_tip = Nc * su_av_tip             [kPa]     95.6    
   Abase = pi * D * D / 4              [m^2]:    28.3    
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Qtip  = eta_REB * Abase * qv_tip     [kN]:   0.270E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:     3635.55916
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     1850.30825
   Qleaking   = Fo                      [kN]:      931.25384
 > Vmax_fun                             [kN]:     1850.30825
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  2
   wt_D_side                             [-]:  0.007
   wt_D_top                              [-]:  0.007
   wt_c = D * wt_D_side                  [m]:  0.039
   wt_x = wt_c                           [m]:  0.039
   wt_t = D * wt_D_top                   [m]:  0.039
   Di = D - 2 * wt_c                     [m]:  5.921
   Awall = Abase - pi*Dinner*Dinner/4  [m^2]:   0.736    
   Axp   = nfnxp * wt_x * Dinner       [m^2]:    0.00    
   Atop  = pi * D * D / 4              [m^2]:    28.3    
   Vst_w = ( Awall + Axp ) * L         [m^3]:    8.83    
   Vst_t =   Atop          * wt_t      [m^3]:    1.11    
   ETA_VST_WALL                          [-]:    1.00    
   Vst   = Vst_w*eta_Vst_wall + Vst_t  [m^3]:    9.94    
   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]:      666.14120
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < 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 =  2
 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   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    2  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    3  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    4  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    5  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    6  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    7  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    8  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
    9  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
   10  1   6.00  12.00   2.00      1850.3      4451.2      1343.5       666.1         6.1
 ----------------------------------------------------------------------------------------
  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   6.00  12.00   9.00  0.00   4026.6   666.1       5  -0.319E-05   ! ? missing text
    2  1   6.00  12.00   9.00 10.00   3752.6   666.1       5  -0.306E-05   ! ? missing text
    3  1   6.00  12.00   9.00 20.00   3501.7   666.1       5  -0.104E-04   ! ? missing text
    4  1   6.00  12.00   9.00 30.00   3247.8   666.1       5  -0.152E-04   ! ? missing text
    5  1   6.00  12.00   9.00 40.00   2983.3   666.1       5  -0.779E-05   ! ? missing text
    6  1   6.00  12.00   9.00 50.00   2748.1   666.1       5  -0.658E-06   ! ? missing text
    7  1   6.00  12.00   9.00 60.00   2567.6   666.1       4  -0.596E-05   ! ? missing text
    8  1   6.00  12.00   9.00 70.00   2447.7   666.1       3   0.902E-06   ! ? missing text
    9  1   6.00  12.00   9.00 80.00   2387.1   666.1       3  -0.823E-05   ! ? missing text
   10  1   6.00  12.00   9.00 90.00   2384.9   666.1       4  -0.116E-05   ! ? missing text
 -----------------------------------------------------------------------
 ilc        D      L    zlug  theta    Tlug     Bw    ( iters    f_VHM )
  icgeom   [m]    [m]   [m]   [deg]    [kN]    [kN]   ( [-]      [-]   )
 -----------------------------------------------------------------------

VHlug_resist_sub: < --- BEGIN
  load case #=    1; caisson geometry #=    1 (#rows results= =  181)
  L         [m] =   12.00
  D         [m] =    6.00
  zlug      [m] =    9.00
  iro_lug   [-] =   1: offset + D/2 (lug on outer face)
  m_fac     [-] =   1.300
  Hmax     [kN] =    0.445E+04
  Vmax     [kN] =    0.185E+04
  theta*        = resistance inclination at lug
  Vlug_theta*, Hlug_theta*
                = corresponding VH FACTORED resistances
  T_theta*      = sqrt( Vlug_theta*^2 + Hlug_theta*^2)
------------------------------------------------------------------------------
 theta*     Vlug_theta*  Hlug_theta*  T_theta*   Vlug_theta*  Hlug_theta*  row
  [deg]        [kN]         [kN]        [kN]      / Vmax [-]   / Hmax [-]  [-]
------------------------------------------------------------------------------
    90.0       0.180E+04   0.110E-12   0.180E+04       0.975    0.000        1
    89.0       0.180E+04    31.5       0.180E+04       0.974    0.007        2
    88.0       0.180E+04    62.9       0.180E+04       0.974    0.014        3
    87.0       0.180E+04    94.4       0.180E+04       0.973    0.021        4
    86.0       0.180E+04    126.       0.180E+04       0.973    0.028        5
    85.0       0.180E+04    157.       0.181E+04       0.972    0.035        6
    84.0       0.180E+04    189.       0.181E+04       0.971    0.042        7
    83.0       0.180E+04    220.       0.181E+04       0.971    0.050        8
    82.0       0.179E+04    252.       0.181E+04       0.970    0.057        9
    81.0       0.179E+04    284.       0.182E+04       0.969    0.064       10
    80.0       0.179E+04    316.       0.182E+04       0.968    0.071       11
    79.0       0.179E+04    348.       0.182E+04       0.967    0.078       12
    78.0       0.179E+04    380.       0.183E+04       0.966    0.085       13
    77.0       0.179E+04    412.       0.183E+04       0.965    0.093       14
    76.0       0.178E+04    445.       0.184E+04       0.965    0.100       15
    75.0       0.178E+04    478.       0.185E+04       0.963    0.107       16
    74.0       0.178E+04    511.       0.185E+04       0.962    0.115       17
    73.0       0.178E+04    544.       0.186E+04       0.961    0.122       18
    72.0       0.178E+04    577.       0.187E+04       0.960    0.130       19
    71.0       0.177E+04    611.       0.188E+04       0.959    0.137       20
    70.0       0.177E+04    645.       0.189E+04       0.958    0.145       21
    69.0       0.177E+04    679.       0.190E+04       0.956    0.153       22
    68.0       0.177E+04    714.       0.191E+04       0.955    0.160       23
    67.0       0.176E+04    749.       0.192E+04       0.954    0.168       24
    66.0       0.176E+04    784.       0.193E+04       0.952    0.176       25
    65.0       0.176E+04    820.       0.194E+04       0.951    0.184       26
    64.0       0.176E+04    856.       0.195E+04       0.949    0.192       27
    63.0       0.175E+04    893.       0.197E+04       0.947    0.201       28
    62.0       0.175E+04    930.       0.198E+04       0.945    0.209       29
    61.0       0.175E+04    968.       0.200E+04       0.943    0.217       30
    60.0       0.174E+04   0.101E+04   0.201E+04       0.941    0.226       31
    59.0       0.174E+04   0.104E+04   0.203E+04       0.939    0.235       32
    58.0       0.173E+04   0.108E+04   0.204E+04       0.937    0.243       33
    57.0       0.173E+04   0.112E+04   0.206E+04       0.935    0.252       34
    56.0       0.172E+04   0.116E+04   0.208E+04       0.932    0.261       35
    55.0       0.172E+04   0.120E+04   0.210E+04       0.930    0.271       36
    54.0       0.171E+04   0.125E+04   0.212E+04       0.927    0.280       37
    53.0       0.171E+04   0.129E+04   0.214E+04       0.924    0.289       38
    52.0       0.170E+04   0.133E+04   0.216E+04       0.921    0.299       39
    51.0       0.170E+04   0.137E+04   0.218E+04       0.918    0.309       40
    50.0       0.169E+04   0.142E+04   0.221E+04       0.914    0.319       41
    49.0       0.168E+04   0.146E+04   0.223E+04       0.911    0.329       42
    48.0       0.168E+04   0.151E+04   0.226E+04       0.907    0.339       43
    47.0       0.167E+04   0.156E+04   0.228E+04       0.903    0.350       44
    46.0       0.166E+04   0.161E+04   0.231E+04       0.898    0.361       45
    45.0       0.165E+04   0.165E+04   0.234E+04       0.894    0.372       46
    44.0       0.164E+04   0.170E+04   0.237E+04       0.889    0.383       47
    43.0       0.164E+04   0.175E+04   0.240E+04       0.884    0.394       48
    42.0       0.163E+04   0.181E+04   0.243E+04       0.878    0.406       49
    41.0       0.161E+04   0.186E+04   0.246E+04       0.873    0.417       50
    40.0       0.160E+04   0.191E+04   0.249E+04       0.866    0.429       51
    39.0       0.159E+04   0.196E+04   0.253E+04       0.860    0.441       52
    38.0       0.158E+04   0.202E+04   0.256E+04       0.853    0.454       53
    37.0       0.156E+04   0.208E+04   0.260E+04       0.845    0.466       54
    36.0       0.155E+04   0.213E+04   0.264E+04       0.838    0.479       55
    35.0       0.153E+04   0.219E+04   0.267E+04       0.829    0.492       56
    34.0       0.152E+04   0.225E+04   0.271E+04       0.820    0.505       57
    33.0       0.150E+04   0.231E+04   0.275E+04       0.811    0.519       58
    32.0       0.148E+04   0.237E+04   0.279E+04       0.800    0.532       59
    31.0       0.146E+04   0.243E+04   0.284E+04       0.789    0.546       60
    30.0       0.144E+04   0.249E+04   0.288E+04       0.778    0.560       61
    29.0       0.142E+04   0.256E+04   0.292E+04       0.766    0.574       62
    28.0       0.139E+04   0.262E+04   0.297E+04       0.752    0.588       63
    27.0       0.137E+04   0.268E+04   0.301E+04       0.738    0.602       64
    26.0       0.134E+04   0.275E+04   0.305E+04       0.724    0.617       65
    25.0       0.131E+04   0.281E+04   0.310E+04       0.708    0.631       66
    24.0       0.128E+04   0.287E+04   0.314E+04       0.691    0.645       67
    23.0       0.125E+04   0.294E+04   0.319E+04       0.674    0.660       68
    22.0       0.121E+04   0.300E+04   0.323E+04       0.655    0.674       69
    21.0       0.118E+04   0.306E+04   0.328E+04       0.635    0.688       70
    20.0       0.114E+04   0.312E+04   0.332E+04       0.614    0.702       71
    19.0       0.110E+04   0.318E+04   0.337E+04       0.593    0.715       72
    18.0       0.105E+04   0.324E+04   0.341E+04       0.570    0.729       73
    17.0       0.101E+04   0.330E+04   0.345E+04       0.546    0.742       74
    16.0        964.       0.336E+04   0.350E+04       0.521    0.755       75
    15.0        916.       0.342E+04   0.354E+04       0.495    0.768       76
    14.0        865.       0.347E+04   0.358E+04       0.468    0.780       77
    13.0        813.       0.352E+04   0.362E+04       0.440    0.792       78
    12.0        760.       0.357E+04   0.365E+04       0.411    0.803       79
    11.0        704.       0.362E+04   0.369E+04       0.381    0.814       80
    10.0        647.       0.367E+04   0.373E+04       0.350    0.825       81
    9.00        588.       0.372E+04   0.376E+04       0.318    0.835       82
    8.00        528.       0.376E+04   0.380E+04       0.286    0.844       83
    7.00        467.       0.380E+04   0.383E+04       0.252    0.854       84
    6.00        404.       0.384E+04   0.386E+04       0.218    0.863       85
    5.00        339.       0.388E+04   0.389E+04       0.183    0.872       86
    4.00        274.       0.392E+04   0.393E+04       0.148    0.880       87
    3.00        207.       0.395E+04   0.396E+04       0.112    0.888       88
    2.00        139.       0.399E+04   0.399E+04       0.075    0.896       89
    1.00        70.2       0.402E+04   0.402E+04       0.038    0.904       90
    0.00        0.00       0.406E+04   0.406E+04       0.000    0.912       91
   -1.00       -71.4       0.409E+04   0.409E+04      -0.039    0.919       92
   -2.00       -144.       0.412E+04   0.413E+04      -0.078    0.926       93
   -3.00       -218.       0.415E+04   0.416E+04      -0.118    0.933       94
   -4.00       -292.       0.418E+04   0.419E+04      -0.158    0.940       95
   -5.00       -368.       0.421E+04   0.423E+04      -0.199    0.946       96
   -6.00       -445.       0.423E+04   0.426E+04      -0.241    0.951       97
   -7.00       -523.       0.426E+04   0.429E+04      -0.282    0.956       98
   -8.00       -600.       0.427E+04   0.431E+04      -0.325    0.960       99
   -9.00       -679.       0.428E+04   0.434E+04      -0.367    0.963      100
   -10.0       -757.       0.429E+04   0.436E+04      -0.409    0.964      101
   -11.0       -834.       0.429E+04   0.437E+04      -0.451    0.964      102
   -12.0       -910.       0.428E+04   0.438E+04      -0.492    0.962      103
   -13.0       -984.       0.426E+04   0.438E+04      -0.532    0.958      104
   -14.0      -0.106E+04   0.424E+04   0.437E+04      -0.571    0.952      105
   -15.0      -0.113E+04   0.420E+04   0.435E+04      -0.609    0.944      106
   -16.0      -0.119E+04   0.416E+04   0.433E+04      -0.644    0.934      107
   -17.0      -0.125E+04   0.410E+04   0.429E+04      -0.678    0.922      108
   -18.0      -0.131E+04   0.404E+04   0.425E+04      -0.710    0.908      109
   -19.0      -0.137E+04   0.397E+04   0.420E+04      -0.739    0.892      110
   -20.0      -0.142E+04   0.389E+04   0.414E+04      -0.765    0.874      111
   -21.0      -0.146E+04   0.381E+04   0.408E+04      -0.790    0.855      112
   -22.0      -0.150E+04   0.372E+04   0.401E+04      -0.812    0.835      113
   -23.0      -0.154E+04   0.363E+04   0.394E+04      -0.832    0.814      114
   -24.0      -0.157E+04   0.353E+04   0.386E+04      -0.849    0.793      115
   -25.0      -0.160E+04   0.343E+04   0.379E+04      -0.865    0.771      116
   -26.0      -0.163E+04   0.333E+04   0.371E+04      -0.879    0.749      117
   -27.0      -0.165E+04   0.324E+04   0.363E+04      -0.891    0.727      118
   -28.0      -0.167E+04   0.314E+04   0.356E+04      -0.902    0.705      119
   -29.0      -0.169E+04   0.304E+04   0.348E+04      -0.912    0.684      120
   -30.0      -0.170E+04   0.295E+04   0.340E+04      -0.920    0.662      121
   -31.0      -0.172E+04   0.286E+04   0.333E+04      -0.927    0.642      122
   -32.0      -0.173E+04   0.277E+04   0.326E+04      -0.934    0.621      123
   -33.0      -0.174E+04   0.268E+04   0.319E+04      -0.940    0.601      124
   -34.0      -0.175E+04   0.259E+04   0.313E+04      -0.945    0.582      125
   -35.0      -0.176E+04   0.251E+04   0.306E+04      -0.949    0.563      126
   -36.0      -0.176E+04   0.243E+04   0.300E+04      -0.953    0.545      127
   -37.0      -0.177E+04   0.235E+04   0.294E+04      -0.956    0.528      128
   -38.0      -0.178E+04   0.227E+04   0.288E+04      -0.959    0.510      129
   -39.0      -0.178E+04   0.220E+04   0.283E+04      -0.962    0.494      130
   -40.0      -0.178E+04   0.213E+04   0.278E+04      -0.965    0.478      131
   -41.0      -0.179E+04   0.206E+04   0.273E+04      -0.967    0.462      132
   -42.0      -0.179E+04   0.199E+04   0.268E+04      -0.969    0.447      133
   -43.0      -0.180E+04   0.193E+04   0.263E+04      -0.970    0.433      134
   -44.0      -0.180E+04   0.186E+04   0.259E+04      -0.972    0.418      135
   -45.0      -0.180E+04   0.180E+04   0.255E+04      -0.973    0.405      136
   -46.0      -0.180E+04   0.174E+04   0.251E+04      -0.974    0.391      137
   -47.0      -0.180E+04   0.168E+04   0.247E+04      -0.975    0.378      138
   -48.0      -0.181E+04   0.163E+04   0.243E+04      -0.976    0.365      139
   -49.0      -0.181E+04   0.157E+04   0.240E+04      -0.977    0.353      140
   -50.0      -0.181E+04   0.152E+04   0.236E+04      -0.978    0.341      141
   -51.0      -0.181E+04   0.147E+04   0.233E+04      -0.978    0.329      142
   -52.0      -0.181E+04   0.142E+04   0.230E+04      -0.979    0.318      143
   -53.0      -0.181E+04   0.137E+04   0.227E+04      -0.980    0.307      144
   -54.0      -0.181E+04   0.132E+04   0.224E+04      -0.980    0.296      145
   -55.0      -0.181E+04   0.127E+04   0.221E+04      -0.980    0.285      146
   -56.0      -0.181E+04   0.122E+04   0.219E+04      -0.981    0.275      147
   -57.0      -0.182E+04   0.118E+04   0.216E+04      -0.981    0.265      148
   -58.0      -0.182E+04   0.113E+04   0.214E+04      -0.981    0.255      149
   -59.0      -0.182E+04   0.109E+04   0.212E+04      -0.981    0.245      150
   -60.0      -0.182E+04   0.105E+04   0.210E+04      -0.982    0.236      151
   -61.0      -0.182E+04   0.101E+04   0.208E+04      -0.982    0.226      152
   -62.0      -0.182E+04    966.       0.206E+04      -0.982    0.217      153
   -63.0      -0.182E+04    926.       0.204E+04      -0.982    0.208      154
   -64.0      -0.182E+04    886.       0.202E+04      -0.982    0.199      155
   -65.0      -0.182E+04    847.       0.200E+04      -0.982    0.190      156
   -66.0      -0.182E+04    809.       0.199E+04      -0.982    0.182      157
   -67.0      -0.182E+04    771.       0.197E+04      -0.982    0.173      158
   -68.0      -0.182E+04    734.       0.196E+04      -0.982    0.165      159
   -69.0      -0.182E+04    697.       0.195E+04      -0.982    0.157      160
   -70.0      -0.182E+04    661.       0.193E+04      -0.982    0.149      161
   -71.0      -0.182E+04    625.       0.192E+04      -0.981    0.140      162
   -72.0      -0.182E+04    590.       0.191E+04      -0.981    0.133      163
   -73.0      -0.182E+04    555.       0.190E+04      -0.981    0.125      164
   -74.0      -0.182E+04    520.       0.189E+04      -0.981    0.117      165
   -75.0      -0.181E+04    486.       0.188E+04      -0.981    0.109      166
   -76.0      -0.181E+04    452.       0.187E+04      -0.980    0.102      167
   -77.0      -0.181E+04    419.       0.186E+04      -0.980    0.094      168
   -78.0      -0.181E+04    385.       0.185E+04      -0.980    0.087      169
   -79.0      -0.181E+04    352.       0.185E+04      -0.980    0.079      170
   -80.0      -0.181E+04    320.       0.184E+04      -0.979    0.072      171
   -81.0      -0.181E+04    287.       0.183E+04      -0.979    0.064      172
   -82.0      -0.181E+04    254.       0.183E+04      -0.979    0.057      173
   -83.0      -0.181E+04    222.       0.182E+04      -0.978    0.050      174
   -84.0      -0.181E+04    190.       0.182E+04      -0.978    0.043      175
   -85.0      -0.181E+04    158.       0.182E+04      -0.977    0.036      176
   -86.0      -0.181E+04    126.       0.181E+04      -0.977    0.028      177
   -87.0      -0.181E+04    94.7       0.181E+04      -0.977    0.021      178
   -88.0      -0.181E+04    63.1       0.181E+04      -0.976    0.014      179
   -89.0      -0.181E+04    31.5       0.181E+04      -0.976    0.007      180
   -90.0      -0.180E+04   0.110E-12   0.180E+04      -0.975    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
