
 p r o g r a m  C A I S S O N _ V H M  w32 version 00.12_b04 
 ------------------------------------  at 11:57:49 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
    1
  zdep        bden       su_top      su_bot   
   [m]     [kN/m^3]      [kPa]        [kPa]   
    0.00        10.0        2.00        125.    
    50.0    
 m_fac
    1.00    
 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
  0    0.00    
 D  L  zlug
   6.00  12.00   8.00
 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    1   0.00
 eta_amh  eta_bmh  eta_phimh
   1.00   1.00   1.00
 ssidat: END --- >


 chndat: < --- BEGIN
 iscope_Bw  l_fac_Bw  eta_Vst_wall  delta_Bw_user  Bw_caisson_user
    0    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 :    3
caisson_vhm: nlines_errors   :    0

WARNING: gmdata. soil layer # 1; BDEN=10.00 kN/m^3 is inconsistent with SU_TOP=2.00 kPa.
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].

solve_MODE22_sub: < --- BEGIN

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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   12014.928
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000       0.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:       0.000
   Hlug=Tlug*cos(theta_lug_star)        [kN]:   12014.928
   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]:       0.000   12014.928  -96119.428
   Vstar,Hstar,Mstar                     [-]:       0.000       9.957      -6.638
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.957      -6.638       0.000
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.966
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.034
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -1.000
 > f_VHM_fun                             [-]: -0.2182304E-05
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   12190.884
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      10.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    2116.925
   Hlug=Tlug*cos(theta_lug_star)        [kN]:   12005.677
   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]:    2116.925   12005.677  -96045.416
   Vstar,Hstar,Mstar                     [-]:       0.194       9.949      -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                  9.949      -6.633       0.194
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.964
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.034
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.998
 > f_VHM_fun                             [-]: -0.2552323E-05
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   12642.893
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      20.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    4324.124
   Hlug=Tlug*cos(theta_lug_star)        [kN]:   11880.434
   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]:    4324.124   11880.434  -95043.469
   Vstar,Hstar,Mstar                     [-]:       0.397       9.845      -6.563
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.845      -6.563       0.397
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.944
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.034
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.978
 > f_VHM_fun                             [-]: -0.1024904E-04
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   13109.036
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      30.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    6554.518
   Hlug=Tlug*cos(theta_lug_star)        [kN]:   11352.758
   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]:    6554.518   11352.758  -90822.066
   Vstar,Hstar,Mstar                     [-]:       0.601       9.408      -6.272
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  9.408      -6.272       0.601
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.862
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.031
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.893
 > f_VHM_fun                             [-]:  0.1833461E-07
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   13187.487
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      40.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    8476.753
   Hlug=Tlug*cos(theta_lug_star)        [kN]:   10102.201
   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]:    8476.753   10102.201  -80817.606
   Vstar,Hstar,Mstar                     [-]:       0.778       8.372      -5.581
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  8.372      -5.581       0.778
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.683
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.024
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.707
 > f_VHM_fun                             [-]: -0.2332576E-04
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   12756.228
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      50.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:    9771.838
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    8199.546
   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]:    9771.838    8199.546  -65596.365
   Vstar,Hstar,Mstar                     [-]:       0.896       6.795      -4.530
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  6.795      -4.530       0.896
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.450
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.016
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.466
 > f_VHM_fun                             [-]: -0.7868624E-05
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   12089.307
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      60.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:   10469.647
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    6044.653
   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]:   10469.647    6044.653  -48357.226
   Vstar,Hstar,Mstar                     [-]:       0.960       5.009      -3.339
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  5.009      -3.339       0.960
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.244
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.009
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.253
 > f_VHM_fun                             [-]: -0.3261181E-05
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   11473.096
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      70.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:   10781.184
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    3924.030
   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]:   10781.184    3924.030  -31392.239
   Vstar,Hstar,Mstar                     [-]:       0.989       3.252      -2.168
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  3.252      -2.168       0.989
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.103
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.004
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.107
 > f_VHM_fun                             [-]: -0.1634410E-03
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:       -0.00016
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < 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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   11057.544
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      80.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:   10889.555
   Hlug=Tlug*cos(theta_lug_star)        [kN]:    1920.122
   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]:   10889.555    1920.122  -15360.979
   Vstar,Hstar,Mstar                     [-]:       0.999       1.591      -1.061
   root_Tlug_22_fun=f_VHM_fun               

f_VHM_fun : < --- BEGIN
 < L,D                                   [m]:   6.00  12.00
   X = Hstar; Y = Mstar; Z = Vstar                  1.591      -1.061       0.999
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.025
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.001
   Z: - (1-(|Z|**bVH))**(2.0d0/aVH)                  [-]:      -0.023
 > f_VHM_fun                             [-]:  0.2993566E-02
f_VHM_fun : END --- >

 > root_Tlug_22_fun                      [-]:        0.00299
root_Tlug_22_fun: END --- >


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < 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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >


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

root_Tlug_22_fun: < --- BEGIN
 < Tlug                                 [kN]:   10902.515
   L , D                                 [m]:      12.000       6.000
   zlug , theta_lug_star           [m] [deg]:       8.000      90.000
   zlug_cL                               [m]:       8.000
   Bw , Bw_plug                         [kN]:       0.000       0.000
   su_av_L                             [kPa]:      16.760
   Vmax                                 [kN]:   10902.515
   Hfac=L   D su_av_L                   [kN]:    1206.720
   Mfac=L^2 D su_av_L                  [kNm]:   14480.640
   aMH , bMH                             [-]:      12.173       1.626
   phiMH , phiMH                 [rad] [deg]:      -0.613     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   Vlug=Tlug*sin(theta_lug_star)        [kN]:   10902.515
   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]:   10902.515       0.000      -0.000
   Vstar,Hstar,Mstar                     [-]:       1.000       0.000      -0.000
   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      -0.000       1.000
   eta_aMH , eta_bMH , eta_phiMH         [-]:       1.000       1.000       1.000
   aMH,bMH,phiMH               [-],[-],[deg]:      12.173       1.626     -35.133
   aMH_new,bMH_new,phiMH_new   [-],[-],[deg]:      12.173       1.626     -35.133
   aVH , bVH                             [-]:       2.858       3.734
   XY:((+cos(phiMH)*X+sin(phiMH)*Y)/aMH)^2           [-]:       0.000
   XY:((-sin(phiMH)*X+cos(phiMH)*Y)/bMH)^2           [-]:       0.000
   Z:|Z| (=|Vstar|) > 1; -(1-|Z|)                    [-]:      -0.000
 > f_VHM_fun                             [-]:  0.3087250E-32
f_VHM_fun : END --- >

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


Vmax_fun : < --- BEGIN
 < support_foundation                  [T/F]: F
 < iplug_vmode                           [-]:  1
 < L,D                                   [m]:  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]:    16.8    
   Fo = eta_Fo*pi*D *L*alpha_Fo*su_av_L [kN]:     2539.98520
   Fi =        pi*Di*L*alpha_Fi*su_av_L [kN]:     2506.71139
   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]:    35.2    
   qv_tip = Nc * su_av_tip             [kPa]     296.    
   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]:   0.836E+04
   Qwall =           Awall * qv_tip     [kN]:    0.00    
   Qxp   =           Axp   * qv_tip     [kN]:    0.00    
   Qplugged   = Fo+Qtip                 [kN]:    10902.51529
   Qunplugged = Fo+Fi+Fxp+Qwall+Qxp     [kN]:     5046.69659
   Qleaking   = Fo                      [kN]:     2539.98520
 > Vmax_fun                             [kN]:    10902.51529
Vmax_fun : END --- >


Bw_caisson_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < iscope_Bw                             [-]:  0
 > Bw_caisson_fun                       [kN]:        0.00000
Bw_caisson_fun : END --- >


Bw_plug_fun : < --- BEGIN
 < L,D                                   [m]:  12.00   6.00
 < wt_D_side (= WT / D)                  [-]:  0.007
 < iplug_Vmode                           [-]:  1
 > Bw_plug_fun                          [kN]:        0.00000
Bw_plug_fun : END --- >



 -----------------------------------------------
 solve_MODE22_sub: CAISSON RESISTANCES & WEIGHTS
 MODE_VHM, problem solution mode =   22
 IPLUG_VMODE, axial capacity mode  =  1
 ISCOPE_BW, caisson weight BW mode =  0
 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     10902.5     12013.8      3409.2         0.0        16.8
    2  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    3  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    4  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    5  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    6  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    7  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    8  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
    9  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
   10  1   6.00  12.00   2.00     10902.5     12013.8      3409.2         0.0        16.8
 ----------------------------------------------------------------------------------------
  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   6.00  12.00   8.00  0.00  12014.9     0.0       5  -0.218E-05   ! ? missing text
    2  1   6.00  12.00   8.00 10.00  12190.9     0.0       5  -0.255E-05   ! ? missing text
    3  1   6.00  12.00   8.00 20.00  12642.9     0.0       5  -0.102E-04   ! ? missing text
    4  1   6.00  12.00   8.00 30.00  13109.0     0.0       6   0.183E-07   ! ? missing text
    5  1   6.00  12.00   8.00 40.00  13187.5     0.0       5  -0.233E-04   ! ? missing text
    6  1   6.00  12.00   8.00 50.00  12756.2     0.0       4  -0.787E-05   ! ? missing text
    7  1   6.00  12.00   8.00 60.00  12089.3     0.0       6  -0.326E-05   ! ? missing text
    8  1   6.00  12.00   8.00 70.00  11473.1     0.0       8  -0.163E-03   ! ? missing text
    9  1   6.00  12.00   8.00 80.00  11057.5     0.0      10   0.299E-02   ! ? missing text
   10  1   6.00  12.00   8.00 90.00  10902.5     0.0       3   0.309E-32   ! ? 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] =    8.00
  iro_lug   [-] =   0: no offset (lug on centreline)
  m_fac     [-] =   1.000
  Hmax     [kN] =    0.120E+05
  Vmax     [kN] =    0.109E+05
  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       0.109E+05   0.668E-12   0.109E+05       1.000    0.000        1
    89.0       0.109E+05    190.       0.109E+05       1.001    0.016        2
    88.0       0.109E+05    381.       0.109E+05       1.002    0.032        3
    87.0       0.109E+05    573.       0.109E+05       1.003    0.048        4
    86.0       0.109E+05    764.       0.109E+05       1.002    0.064        5
    85.0       0.109E+05    954.       0.109E+05       1.000    0.079        6
    84.0       0.109E+05   0.114E+04   0.110E+05       0.999    0.095        7
    83.0       0.109E+05   0.134E+04   0.110E+05       0.999    0.111        8
    82.0       0.109E+05   0.153E+04   0.110E+05       0.999    0.127        9
    81.0       0.109E+05   0.173E+04   0.110E+05       0.999    0.144       10
    80.0       0.109E+05   0.192E+04   0.111E+05       0.999    0.160       11
    79.0       0.109E+05   0.212E+04   0.111E+05       0.998    0.176       12
    78.0       0.109E+05   0.231E+04   0.111E+05       0.998    0.192       13
    77.0       0.109E+05   0.251E+04   0.112E+05       0.997    0.209       14
    76.0       0.109E+05   0.271E+04   0.112E+05       0.996    0.225       15
    75.0       0.109E+05   0.291E+04   0.112E+05       0.995    0.242       16
    74.0       0.108E+05   0.311E+04   0.113E+05       0.994    0.259       17
    73.0       0.108E+05   0.331E+04   0.113E+05       0.993    0.276       18
    72.0       0.108E+05   0.351E+04   0.114E+05       0.992    0.292       19
    71.0       0.108E+05   0.372E+04   0.114E+05       0.990    0.309       20
    70.0       0.108E+05   0.392E+04   0.115E+05       0.989    0.327       21
    69.0       0.108E+05   0.413E+04   0.115E+05       0.987    0.344       22
    68.0       0.107E+05   0.434E+04   0.116E+05       0.985    0.361       23
    67.0       0.107E+05   0.455E+04   0.116E+05       0.983    0.379       24
    66.0       0.107E+05   0.476E+04   0.117E+05       0.980    0.396       25
    65.0       0.107E+05   0.497E+04   0.118E+05       0.978    0.414       26
    64.0       0.106E+05   0.518E+04   0.118E+05       0.975    0.432       27
    63.0       0.106E+05   0.540E+04   0.119E+05       0.972    0.449       28
    62.0       0.106E+05   0.561E+04   0.120E+05       0.968    0.467       29
    61.0       0.105E+05   0.583E+04   0.120E+05       0.964    0.485       30
    60.0       0.105E+05   0.604E+04   0.121E+05       0.960    0.503       31
    59.0       0.104E+05   0.626E+04   0.122E+05       0.956    0.521       32
    58.0       0.104E+05   0.648E+04   0.122E+05       0.951    0.539       33
    57.0       0.103E+05   0.670E+04   0.123E+05       0.946    0.557       34
    56.0       0.102E+05   0.691E+04   0.124E+05       0.940    0.575       35
    55.0       0.102E+05   0.713E+04   0.124E+05       0.934    0.593       36
    54.0       0.101E+05   0.735E+04   0.125E+05       0.927    0.612       37
    53.0       0.100E+05   0.756E+04   0.126E+05       0.920    0.629       38
    52.0       0.995E+04   0.778E+04   0.126E+05       0.913    0.647       39
    51.0       0.987E+04   0.799E+04   0.127E+05       0.905    0.665       40
    50.0       0.977E+04   0.820E+04   0.128E+05       0.896    0.683       41
    49.0       0.967E+04   0.841E+04   0.128E+05       0.887    0.700       42
    48.0       0.957E+04   0.861E+04   0.129E+05       0.877    0.717       43
    47.0       0.945E+04   0.882E+04   0.129E+05       0.867    0.734       44
    46.0       0.933E+04   0.901E+04   0.130E+05       0.856    0.750       45
    45.0       0.921E+04   0.921E+04   0.130E+05       0.845    0.767       46
    44.0       0.908E+04   0.940E+04   0.131E+05       0.832    0.782       47
    43.0       0.894E+04   0.958E+04   0.131E+05       0.820    0.798       48
    42.0       0.879E+04   0.976E+04   0.131E+05       0.806    0.813       49
    41.0       0.864E+04   0.994E+04   0.132E+05       0.792    0.827       50
    40.0       0.848E+04   0.101E+05   0.132E+05       0.778    0.841       51
    39.0       0.831E+04   0.103E+05   0.132E+05       0.762    0.854       52
    38.0       0.814E+04   0.104E+05   0.132E+05       0.746    0.867       53
    37.0       0.796E+04   0.106E+05   0.132E+05       0.730    0.879       54
    36.0       0.777E+04   0.107E+05   0.132E+05       0.713    0.890       55
    35.0       0.758E+04   0.108E+05   0.132E+05       0.695    0.901       56
    34.0       0.738E+04   0.109E+05   0.132E+05       0.677    0.911       57
    33.0       0.718E+04   0.111E+05   0.132E+05       0.659    0.921       58
    32.0       0.698E+04   0.112E+05   0.132E+05       0.640    0.929       59
    31.0       0.677E+04   0.113E+05   0.131E+05       0.621    0.938       60
    30.0       0.655E+04   0.114E+05   0.131E+05       0.601    0.945       61
    29.0       0.634E+04   0.114E+05   0.131E+05       0.581    0.952       62
    28.0       0.612E+04   0.115E+05   0.130E+05       0.561    0.958       63
    27.0       0.590E+04   0.116E+05   0.130E+05       0.541    0.964       64
    26.0       0.568E+04   0.116E+05   0.129E+05       0.521    0.969       65
    25.0       0.545E+04   0.117E+05   0.129E+05       0.500    0.973       66
    24.0       0.523E+04   0.117E+05   0.128E+05       0.479    0.977       67
    23.0       0.500E+04   0.118E+05   0.128E+05       0.459    0.981       68
    22.0       0.478E+04   0.118E+05   0.127E+05       0.438    0.984       69
    21.0       0.455E+04   0.119E+05   0.127E+05       0.417    0.987       70
    20.0       0.432E+04   0.119E+05   0.126E+05       0.397    0.989       71
    19.0       0.410E+04   0.119E+05   0.126E+05       0.376    0.991       72
    18.0       0.387E+04   0.119E+05   0.125E+05       0.355    0.993       73
    17.0       0.365E+04   0.119E+05   0.125E+05       0.335    0.994       74
    16.0       0.343E+04   0.120E+05   0.124E+05       0.315    0.995       75
    15.0       0.321E+04   0.120E+05   0.124E+05       0.294    0.996       76
    14.0       0.299E+04   0.120E+05   0.123E+05       0.274    0.997       77
    13.0       0.277E+04   0.120E+05   0.123E+05       0.254    0.998       78
    12.0       0.255E+04   0.120E+05   0.123E+05       0.234    0.999       79
    11.0       0.233E+04   0.120E+05   0.122E+05       0.214    0.999       80
    10.0       0.212E+04   0.120E+05   0.122E+05       0.194    0.999       81
    9.00       0.190E+04   0.120E+05   0.122E+05       0.174    1.000       82
    8.00       0.169E+04   0.120E+05   0.121E+05       0.155    1.000       83
    7.00       0.147E+04   0.120E+05   0.121E+05       0.135    1.000       84
    6.00       0.126E+04   0.120E+05   0.121E+05       0.116    1.000       85
    5.00       0.105E+04   0.120E+05   0.121E+05       0.096    1.000       86
    4.00        840.       0.120E+05   0.120E+05       0.077    1.000       87
    3.00        630.       0.120E+05   0.120E+05       0.058    1.000       88
    2.00        420.       0.120E+05   0.120E+05       0.038    1.000       89
    1.00        210.       0.120E+05   0.120E+05       0.019    1.000       90
    0.00        0.00       0.120E+05   0.120E+05       0.000    1.000       91
   -1.00       -210.       0.120E+05   0.120E+05      -0.019    1.000       92
   -2.00       -420.       0.120E+05   0.120E+05      -0.038    1.000       93
   -3.00       -630.       0.120E+05   0.120E+05      -0.058    1.000       94
   -4.00       -840.       0.120E+05   0.120E+05      -0.077    1.000       95
   -5.00      -0.105E+04   0.120E+05   0.121E+05      -0.096    1.000       96
   -6.00      -0.126E+04   0.120E+05   0.121E+05      -0.116    1.000       97
   -7.00      -0.147E+04   0.120E+05   0.121E+05      -0.135    1.000       98
   -8.00      -0.169E+04   0.120E+05   0.121E+05      -0.155    1.000       99
   -9.00      -0.190E+04   0.120E+05   0.122E+05      -0.174    1.000      100
   -10.0      -0.212E+04   0.120E+05   0.122E+05      -0.194    0.999      101
   -11.0      -0.233E+04   0.120E+05   0.122E+05      -0.214    0.999      102
   -12.0      -0.255E+04   0.120E+05   0.123E+05      -0.234    0.999      103
   -13.0      -0.277E+04   0.120E+05   0.123E+05      -0.254    0.998      104
   -14.0      -0.299E+04   0.120E+05   0.123E+05      -0.274    0.997      105
   -15.0      -0.321E+04   0.120E+05   0.124E+05      -0.294    0.996      106
   -16.0      -0.343E+04   0.120E+05   0.124E+05      -0.315    0.995      107
   -17.0      -0.365E+04   0.119E+05   0.125E+05      -0.335    0.994      108
   -18.0      -0.387E+04   0.119E+05   0.125E+05      -0.355    0.993      109
   -19.0      -0.410E+04   0.119E+05   0.126E+05      -0.376    0.991      110
   -20.0      -0.432E+04   0.119E+05   0.126E+05      -0.397    0.989      111
   -21.0      -0.455E+04   0.119E+05   0.127E+05      -0.417    0.987      112
   -22.0      -0.478E+04   0.118E+05   0.127E+05      -0.438    0.984      113
   -23.0      -0.500E+04   0.118E+05   0.128E+05      -0.459    0.981      114
   -24.0      -0.523E+04   0.117E+05   0.128E+05      -0.479    0.977      115
   -25.0      -0.545E+04   0.117E+05   0.129E+05      -0.500    0.973      116
   -26.0      -0.568E+04   0.116E+05   0.129E+05      -0.521    0.969      117
   -27.0      -0.590E+04   0.116E+05   0.130E+05      -0.541    0.964      118
   -28.0      -0.612E+04   0.115E+05   0.130E+05      -0.561    0.958      119
   -29.0      -0.634E+04   0.114E+05   0.131E+05      -0.581    0.952      120
   -30.0      -0.655E+04   0.114E+05   0.131E+05      -0.601    0.945      121
   -31.0      -0.677E+04   0.113E+05   0.131E+05      -0.621    0.938      122
   -32.0      -0.698E+04   0.112E+05   0.132E+05      -0.640    0.929      123
   -33.0      -0.718E+04   0.111E+05   0.132E+05      -0.659    0.921      124
   -34.0      -0.738E+04   0.109E+05   0.132E+05      -0.677    0.911      125
   -35.0      -0.758E+04   0.108E+05   0.132E+05      -0.695    0.901      126
   -36.0      -0.777E+04   0.107E+05   0.132E+05      -0.713    0.890      127
   -37.0      -0.796E+04   0.106E+05   0.132E+05      -0.730    0.879      128
   -38.0      -0.814E+04   0.104E+05   0.132E+05      -0.746    0.867      129
   -39.0      -0.831E+04   0.103E+05   0.132E+05      -0.762    0.854      130
   -40.0      -0.848E+04   0.101E+05   0.132E+05      -0.778    0.841      131
   -41.0      -0.864E+04   0.994E+04   0.132E+05      -0.792    0.827      132
   -42.0      -0.879E+04   0.976E+04   0.131E+05      -0.806    0.813      133
   -43.0      -0.894E+04   0.958E+04   0.131E+05      -0.820    0.798      134
   -44.0      -0.908E+04   0.940E+04   0.131E+05      -0.832    0.782      135
   -45.0      -0.921E+04   0.921E+04   0.130E+05      -0.845    0.767      136
   -46.0      -0.933E+04   0.901E+04   0.130E+05      -0.856    0.750      137
   -47.0      -0.945E+04   0.882E+04   0.129E+05      -0.867    0.734      138
   -48.0      -0.957E+04   0.861E+04   0.129E+05      -0.877    0.717      139
   -49.0      -0.967E+04   0.841E+04   0.128E+05      -0.887    0.700      140
   -50.0      -0.977E+04   0.820E+04   0.128E+05      -0.896    0.683      141
   -51.0      -0.987E+04   0.799E+04   0.127E+05      -0.905    0.665      142
   -52.0      -0.995E+04   0.778E+04   0.126E+05      -0.913    0.647      143
   -53.0      -0.100E+05   0.756E+04   0.126E+05      -0.920    0.629      144
   -54.0      -0.101E+05   0.735E+04   0.125E+05      -0.927    0.612      145
   -55.0      -0.102E+05   0.713E+04   0.124E+05      -0.934    0.593      146
   -56.0      -0.102E+05   0.691E+04   0.124E+05      -0.940    0.575      147
   -57.0      -0.103E+05   0.670E+04   0.123E+05      -0.946    0.557      148
   -58.0      -0.104E+05   0.648E+04   0.122E+05      -0.951    0.539      149
   -59.0      -0.104E+05   0.626E+04   0.122E+05      -0.956    0.521      150
   -60.0      -0.105E+05   0.604E+04   0.121E+05      -0.960    0.503      151
   -61.0      -0.105E+05   0.583E+04   0.120E+05      -0.964    0.485      152
   -62.0      -0.106E+05   0.561E+04   0.120E+05      -0.968    0.467      153
   -63.0      -0.106E+05   0.540E+04   0.119E+05      -0.972    0.449      154
   -64.0      -0.106E+05   0.518E+04   0.118E+05      -0.975    0.432      155
   -65.0      -0.107E+05   0.497E+04   0.118E+05      -0.978    0.414      156
   -66.0      -0.107E+05   0.476E+04   0.117E+05      -0.980    0.396      157
   -67.0      -0.107E+05   0.455E+04   0.116E+05      -0.983    0.379      158
   -68.0      -0.107E+05   0.434E+04   0.116E+05      -0.985    0.361      159
   -69.0      -0.108E+05   0.413E+04   0.115E+05      -0.987    0.344      160
   -70.0      -0.108E+05   0.392E+04   0.115E+05      -0.989    0.327      161
   -71.0      -0.108E+05   0.372E+04   0.114E+05      -0.990    0.309      162
   -72.0      -0.108E+05   0.351E+04   0.114E+05      -0.992    0.292      163
   -73.0      -0.108E+05   0.331E+04   0.113E+05      -0.993    0.276      164
   -74.0      -0.108E+05   0.311E+04   0.113E+05      -0.994    0.259      165
   -75.0      -0.109E+05   0.291E+04   0.112E+05      -0.995    0.242      166
   -76.0      -0.109E+05   0.271E+04   0.112E+05      -0.996    0.225      167
   -77.0      -0.109E+05   0.251E+04   0.112E+05      -0.997    0.209      168
   -78.0      -0.109E+05   0.231E+04   0.111E+05      -0.998    0.192      169
   -79.0      -0.109E+05   0.212E+04   0.111E+05      -0.998    0.176      170
   -80.0      -0.109E+05   0.192E+04   0.111E+05      -0.999    0.160      171
   -81.0      -0.109E+05   0.173E+04   0.110E+05      -0.999    0.144      172
   -82.0      -0.109E+05   0.153E+04   0.110E+05      -0.999    0.127      173
   -83.0      -0.109E+05   0.134E+04   0.110E+05      -0.999    0.111      174
   -84.0      -0.109E+05   0.114E+04   0.110E+05      -0.999    0.095      175
   -85.0      -0.109E+05    954.       0.109E+05      -1.000    0.079      176
   -86.0      -0.109E+05    764.       0.109E+05      -1.002    0.064      177
   -87.0      -0.109E+05    573.       0.109E+05      -1.003    0.048      178
   -88.0      -0.109E+05    381.       0.109E+05      -1.002    0.032      179
   -89.0      -0.109E+05    190.       0.109E+05      -1.001    0.016      180
   -90.0      -0.109E+05   0.668E-12   0.109E+05      -1.000    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
