From c687be42c85249783697093df13ccb9fa12c7043 Mon Sep 17 00:00:00 2001 From: madsmpedersen <m@madsp.dk> Date: Fri, 19 Feb 2016 15:13:15 +0100 Subject: [PATCH] add missing file --- wetb/hawc2/tests/test_files/htcfiles/ansi.htc | 598 ++++++++++++++++++ 1 file changed, 598 insertions(+) create mode 100644 wetb/hawc2/tests/test_files/htcfiles/ansi.htc diff --git a/wetb/hawc2/tests/test_files/htcfiles/ansi.htc b/wetb/hawc2/tests/test_files/htcfiles/ansi.htc new file mode 100644 index 0000000..ed7cd5f --- /dev/null +++ b/wetb/hawc2/tests/test_files/htcfiles/ansi.htc @@ -0,0 +1,598 @@ +;oc4_jacket_phase_1 version 3, 31-01-13, Larh +begin Simulation; + time_stop 200 ; + solvertype 1 ; (newmark) + on_no_convergence continue ; +; convergence_limits 3E4 1.0 0.7 ; + convergence_limits 5E3 1.0 0.7 ; + logfile ./log/oc4_load_case_5-7.log ; + animation ./anim/oc4_jacket.dat; + visualization ./visualization/structure_jacket_new.hdf5; + begin newmark; + deltat .025; + end newmark; +end simulation; +; +begin new_htc_structure; +; beam_output_file_name ./log/oc4_load_case_5-7_beam.dat; Optional - Calculated beam properties of the bodies are written to file +; body_output_file_name ./log/oc4_load_case_5-7_body.dat; Optional - Body initial position and orientation are written to file +; struct_inertia_output_file_name ./log/oc4_load_case_5-7_struct.dat; +; body_eigenanalysis_file_name ./eigenfrq/oc4_load_case_5-7_body_eigen.dat; +; structure_eigenanalysis_file_name ./eigenfrq/oc4_load_case_5-7_strc_eigen.dat ; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +; +; continue_in_file bodies.dat; Definition of substructure +; + begin main_body; tower 68m + name tower ; + type timoschenko ; + nbodies 1 ; + node_distribution c2_def ; + damping_posdef 0.0 0.0 0.0 4.24E-3 4.24E-3 1.25E-3 ; Mx My Mz Kx Ky Kz , M´s raises overall level, K´s raises high freguency level + concentrated_mass 1 0.0 0.0 0.0 1.9E3 0.0 0.0 0.0 ; 1st tower point mass + concentrated_mass 5 0.0 0.0 0.0 1.4E3 0.0 0.0 0.0 ; 2nd tower point mass + concentrated_mass 9 0.0 0.0 0.0 1.0E3 0.0 0.0 0.0 ; 3rd tower point mass + concentrated_mass 1 0.0 0.0 2.0 6.66E5 6.00288E6 6.00288E6 1.02298E7; concrete transition pieace + gravity 9.80665; + begin timoschenko_input; + filename ./data_turb/NREL_5MW_st.txt ; + set 1 1 ; + end timoschenko_input; + begin c2_def; Definition of centerline (main_body coordinates) + nsec 9; + sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist + sec 2 0.0 0.0 -1.0 0.0 ; + sec 3 0.0 0.0 -12.0 0.0 ; + sec 4 0.0 0.0 -22.0 0.0 ; + sec 5 0.0 0.0 -34.0 0.0 ; + sec 6 0.0 0.0 -44.0 0.0 ; + sec 7 0.0 0.0 -54.0 0.0 ; + sec 8 0.0 0.0 -63.0 0.0 ; + sec 9 0.0 0.0 -68.0 0.0 ; + end c2_def ; + end main_body; +; + begin main_body; + name tow_dummy ; Dummy structure with other element coordinate than the tower, for output only + type timoschenko ; + nbodies 1 ; + node_distribution c2_def ; + damping_posdef 0.0 0.0 0.0 3.00E-06 3.00E-06 2.00E-05; + gravity 9.80665; + begin timoschenko_input; + filename ./data_turb/NREL_5MW_st.txt ; + set 4 2 ; + end timoschenko_input; + begin c2_def; Definition of centerline (main_body coordinates) + nsec 2; + sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist + sec 2 0.0 0.0 0.1 0.0 ; + end c2_def ; + end main_body; +; + begin main_body; + name towertop ; + type timoschenko ; + nbodies 1 ; + node_distribution c2_def ; + damping_posdef 0.0 0.0 0.0 3.00E-05 3.00E-05 2.00E-04 ; + concentrated_mass 2 0.0 1.9 0.21256 2.4E5 1741490.0 1.7E5 1741490.0 ; Nacelle mass and inertia + gravity 9.80665; + begin timoschenko_input; + filename ./data_turb/NREL_5MW_st.txt ; + set 2 1 ; + end timoschenko_input; + begin c2_def; Definition of centerline (main_body coordinates) + nsec 2; + sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist + sec 2 0.0 0.0 -1.96256 0.0 ; + end c2_def ; + end main_body; +; + begin main_body; + name shaft ; + type timoschenko ; + nbodies 1 ; + node_distribution c2_def ; + damping_posdef 0.0 0.0 0.0 4.65E-04 4.65E-04 7.0725E-03 ; "tuned by Anyd 23/5/13 to 31.45 log decr. damping for free free with stiff rotor and tower" + concentrated_mass 1 0.0 0.0 0.0 0.0 0.0 0.0 5025497.444 ;generator equivalent slow shaft + concentrated_mass 5 0.0 0.0 0.0 56780 0.0 0.0 115926 ; hub mass and inertia; + gravity 9.80665; + begin timoschenko_input; + filename ./data_turb/NREL_5MW_st.txt ; + set 3 1 ; + end timoschenko_input; + begin c2_def; Definition of centerline (main_body coordinates) + nsec 10; + sec 1 0.0 0.0 0.0 0.0; + sec 2 0.0 0.0 0.2 0.0; + sec 3 0.0 0.0 1.0 0.0 ; Tower top x,y,z,twist + sec 4 0.0 0.0 5.0 0.0 ; + sec 5 0.0 0.0 6.0 0.0 ; + sec 6 0.0 0.0 7.1071 0.0 ; Main bearing + sec 7 0.0 0.0 9.0191 0.0 ; Rotor centre + sec 8 0.0 0.0 11.0 0.0; + sec 9 0.0 0.0 12.5 0; + sec 10 0 0 13.5 0; + end c2_def ; + begin visualization_profile; + type cylinder; + nsec 5; + sec 0 0.0; + sec 0.3 5; + sec 10 5; + sec 11 2; + sec 11.5 0; + end visualization_profile; + end main_body; +; + begin main_body; + name hub1 ; + type timoschenko ; + nbodies 1 ; + node_distribution c2_def ; + damping_posdef 0.0 0.0 0.0 3.00E-06 3.00E-06 2.00E-05; + gravity 9.80665; + begin timoschenko_input; + filename ./data_turb/NREL_5MW_st.txt ; + set 4 1 ; + end timoschenko_input; + begin c2_def; Definition of centerline (main_body coordinates) + nsec 2; + sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist + sec 2 0.0 0.0 1.5 0.0 ; + end c2_def ; + end main_body; +; + begin main_body; + name hub2 ; + copy_main_body hub1; + end main_body; +; + begin main_body; + name hub3 ; + copy_main_body hub1 ; + end main_body; +; + begin main_body; + name blade1 ; + type timoschenko ; + nbodies 9 ; + node_distribution c2_def; + damping_posdef 0.0 0.0 0.0 1.41E-03 2.39E-03 4.5E-05 ; + gravity 9.80665; + begin timoschenko_input ; + filename ./data_turb/NREL_5MW_st.txt ; + set 5 1 ; set subset + end timoschenko_input; + begin c2_def; Definition of centerline (main_body coordinates) + nsec 19 ; + sec 1 0.0000 0.0000 0.000 0.000 ; x.y.z. twist + sec 2 -0.0027 0.0006 1.367 -13.308 ; + sec 3 -0.1057 0.0250 4.100 -13.308 ; + sec 4 -0.2501 0.0592 6.833 -13.308 ; + sec 5 -0.4592 0.1086 10.250 -13.308 ; + sec 6 -0.5699 0.1157 14.350 -11.480 ; + sec 7 -0.5485 0.0983 18.450 -10.162 ; + sec 8 -0.5246 0.0832 22.550 -9.011 ; + sec 9 -0.4962 0.0679 26.650 -7.795 ; + sec 10 -0.4654 0.0534 30.750 -6.544 ; 50% blade radius + sec 11 -0.4358 0.0409 34.850 -5.361 ; + sec 12 -0.4059 0.0297 38.950 -4.188 ; + sec 13 -0.3757 0.0205 43.050 -3.125 ; + sec 14 -0.3452 0.0140 47.150 -2.319 ; + sec 15 -0.3146 0.0084 51.250 -1.526 ; + sec 16 -0.2891 0.0044 54.667 -0.863 ; + sec 17 -0.2607 0.0017 57.400 -0.370 ; + sec 18 -0.1774 0.0003 60.133 -0.106 ; + sec 19 -0.1201 0.0000 61.500 -0.000 ; + end c2_def ; + end main_body; +; + begin main_body; + name blade2 ; + copy_main_body blade1; + end main_body; +; + begin main_body; + name blade3 ; + copy_main_body blade1 ; + end main_body; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- + begin orientation; + ; continue_in_file orientation.dat; +; + begin base; + body tower; + inipos 0.0 0.0 -20.15 ; initial position of node 1 + body_eulerang 0.0 0.0 0.0; + end base; +; + begin relative; + body1 tower 1; + body2 tow_dummy 1; + body2_eulerang 0.0 0.0 0.0; + end relative; +; + begin relative; + body1 tower last; + body2 towertop 1; + body2_eulerang 0.0 0.0 0.0; + end relative; +; + begin relative; + body1 towertop last; + body2 shaft 4; + body2_eulerang 0.0 0.0 0.0; + body2_eulerang 90.0 0.0 0.0; + body2_eulerang 5.0 0.0 0.0; 5 deg tilt angle + body2_ini_rotvec_d1 0.0 0.0 -1.0 1.267109036 ; 12.1 rpm body initial rotation velocity x.y.z.angle velocity[rad/s] (body 2 coordinates) + end relative; +; + begin relative; + body1 shaft 7; + body2 hub1 1; + body2_eulerang -90.0 0.0 0.0; + body2_eulerang 0.0 180.0 0.0; + body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle + end relative; +; + begin relative; + body1 shaft 7; + body2 hub2 1; + body2_eulerang -90.0 0.0 0.0; + body2_eulerang 0.0 60.0 0.0; + body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle + end relative; +; + begin relative; + body1 shaft 7; + body2 hub3 1; + body2_eulerang -90.0 0.0 0.0; + body2_eulerang 0.0 -60.0 0.0; + body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle + end relative; +; + begin relative; + body1 hub1 last; + body2 blade1 1; + body2_eulerang 0.0 0.0 0; + end relative; +; + begin relative; + body1 hub2 last; + body2 blade2 1; + body2_eulerang 0.0 0.0 0.0; + end relative; +; + begin relative; + body1 hub3 last; + body2 blade3 1; + body2_eulerang 0.0 0.0 0.0; + end relative; +; + end orientation; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +begin constraint; +; continue_in_file constraints.dat; +; constraints upper nodes of substructures to tower +; + begin fix1; + mbdy1 T1 1; + mbdy2 tower 1; + end fix1; +; + begin fix1; + mbdy1 T2 1; + mbdy2 tower 1; + end fix1; +; + begin fix1; + mbdy1 T3 1; + mbdy2 tower 1; + end fix1; +; + begin fix1; + mbdy1 T4 1; + mbdy2 tower 1; + end fix1; +; + begin fix1; + mbdy1 tower 1; + mbdy2 tow_dummy 1; + end fix1; +; +; constraints turbine' +; + begin fix1; + body1 tower last ; + body2 towertop 1; + end fix1; +; + begin bearing1; free bearing + name shaft_rot; + body1 towertop last; + body2 shaft 3; + bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present + end bearing1; +; ; + ; begin fix1; + ; body1 towertop last ; + ; body2 shaft 1; + ; end fix1; +; ; + begin fix1; + body1 shaft 8 ; + body2 hub1 1; + end fix1; +; + begin fix1; + body1 shaft 8 ; + body2 hub2 1; + end fix1; +; + begin fix1; + body1 shaft 8 ; + body2 hub3 1; + end fix1; +; + begin bearing2; + name pitch1; + body1 hub1 last; + body2 blade1 1; + bearing_vector 2 0.0 0.0 -1.0; + end bearing2; +; + begin bearing2; + name pitch2; + body1 hub2 last; + body2 blade2 1; + bearing_vector 2 0.0 0.0 -1.0; + end bearing2; +; + begin bearing2; + name pitch3; + body1 hub3 last; + body2 blade3 1; + bearing_vector 2 0.0 0.0 -1.0; + end bearing2; +; +; begin fix1; +; body1 hub1 last ; +; body2 blade1 1; +; end fix1; +; +; begin fix1; +; body1 hub2 last ; +; body2 blade2 1; +; end fix1; +; +; begin fix1; +; body1 hub3 last ; +; body2 blade3 1; +; end fix1; +; +end constraint; +; +end new_htc_structure; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +begin wind ; + density 1.225 ; to be checked + wsp 12.0 ; + tint 0.0; + horizontal_input 1 ; 0=false, 1=true + windfield_rotations 0.0 0.0 0.0 ; yaw, tilt, rotation + center_pos0 0.0 0.0 -90.55; + shear_format 1 0.14 ;0=none,1=constant,2=log,3=power,4=linear + turb_format 0 ; 0=none, 1=mann,2=flex + tower_shadow_method 3 ; 0=none, 1=potential flow, 2=jet +; scale_time_start 0 ; +; wind_ramp_factor 0.0 [t0] [wsp factor] 1.0 ; +; [gust] iec_gust [gust_type] [gust_A] [gust_phi0] [gust_t0] [gust_T] ; +; + begin mann; + filename_u ./turb/dummyu.bin ; + filename_v ./turb/dummyv.bin ; + filename_w ./turb/dummyw.bin ; + box_dim_u 8192 0.0 ; + box_dim_v 32 4.6875; + box_dim_w 32 4.6875; + std_scaling 1.0 0.7 0.5 ; + end mann; +; + begin tower_shadow_potential_2; + tower_mbdy_link tower ; + nsec 2; + radius 0 2.8 ; + radius 68 2.0 ; + end tower_shadow_potential; +end wind; +; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +; +begin aero ; + nblades 3; + hub_vec shaft -3 ; rotor rotation vector (normally shaft composant directed from pressure to sustion side) + link 1 mbdy_c2_def blade1; + link 2 mbdy_c2_def blade2; + link 3 mbdy_c2_def blade3; + ae_filename ./data_turb/NREL_5MW_ae.txt; + pc_filename ./data_turb/NREL_5MW_pc.txt; + induction_method 1 ; 0=none, 1=normal + aerocalc_method 1 ; 0=ingen aerodynamic, 1=med aerodynamic + aerosections 30 ; + ae_sets 1 1 1; + tiploss_method 1 ; 0=none, 1=prandtl + dynstall_method 2 ; 0=none, 1=stig øye method,2=mhh method +end aero ; +; +; begin aerodrag ; + ; begin aerodrag_element ; + ; mbdy_name tower; + ; aerodrag_sections uniform 10 ; + ; nsec 2 ; + ; sec 0.0 0.6 5.6 ; tower bottom + ; sec 87.6 0.6 4.0 ; tower top + ; end aerodrag_element; +; ; + ; begin aerodrag_element ; Nacelle drag side + ; mbdy_name shaft; + ; aerodrag_sections uniform 2 ; + ; nsec 2 ; + ; sec 0.0 0.8 10.0 ; + ; sec 5.02 0.8 10.0 ; + ; end aerodrag_element; +; end aerodrag; +; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +begin dll; + begin hawc_dll; + filename ./control/bladed2hawc.dll ; + dll_subroutine regulation ; + arraysizes 15 15 ; + begin output; + general time ; 1 + constraint bearing2 pitch1 1; angle and angle velocity written to dll 2,3 + constraint bearing2 pitch2 1; angle and angle velocity written to dll 4,5 + constraint bearing2 pitch3 1; angle and angle velocity written to dll 6,7 + constraint bearing2 shaft_rot 1; angle and angle velocity written to dll (slow speed shaft) 8,9 + wind free_wind 1 0.0 0.0 -90.55; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z 10,11,12 + general constant 97.0 ; generator exchange ratio 13 + end output; +; + begin actions; + body moment_ext shaft 1 3; + end actions; + end hawc_dll; +; + begin hawc_dll; + filename ./control/pitchservo_pos.dll ; + dll_subroutine servo ; + arraysizes 15 15 ; + begin output; + general time ; 1 + dll inpvec 1 2; 2 + dll inpvec 1 3; 3 + dll inpvec 1 4; 4 + constraint bearing2 pitch1 1; angle and angle velocity written to dll 5,6 + constraint bearing2 pitch2 1; angle and angle velocity written to dll 7,8 + constraint bearing2 pitch3 1; angle and angle velocity written to dll 9,10 + end output; +; + begin actions; + body bearing_angle pitch1; + body bearing_angle pitch2; + body bearing_angle pitch3; + end actions; + end hawc_dll; +; + ; begin hawc_dll; + ; filename ./control/damper.dll ; + ; dll_subroutine damp ; + ; arraysizes 15 15 ; + ; begin output; + ; general time ; 1 + ; general constant 5.0; + ; general constant 25.0; + ; general constant 0.0 ; + ; mbdy state vel towertop 1 1.0 tower; + ; end output; +; ; + ; begin actions; + ; mbdy force_ext towertop 2 1 towertop; + ; mbdy force_ext towertop 2 2 towertop; + ; end actions; + ; end hawc_dll; +; +; + begin type2_dll; + name gear; + filename ./control/hss_convert.dll ; + arraysizes_init 3 1 ; + arraysizes_update 2 2 ; + begin init; + constant 1 1.0 ; number of used sensors - in this case only 1 + constant 2 1000; unit conversion factor + end init; + begin output; + mbdy momentvec shaft 1 1 shaft # only 3; + end output; +; + begin actions; + mbdy moment_ext towertop 2 3 shaft; + end actions; + end type2_dll; +; +end dll; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +begin HYDRO ; + begin WATER_PROPERTIES ; + rho 1025 ; [kg/m^3] + gravity 9.80665 ; [m/s^2] + mwl 0.00 ; [m] + mudlevel 200 ; [m] + water_kinematics_dll ./wkin_dll.dll ./htc_hydro/ireg_airy_h6_t10.inp ; + end WATER_PROPERTIES ; + ;continue_in_file hydro.dat; + end HYDRO ; +;---------------------------------------------------------------------------------------------------------------------------------------------------------------- +begin output; + filename ./res/oc4_jacket ; + data_format hawc_binary; +; time 50.0 650.0 ; + buffer 1 ; +; + general time; + wind free_wind 1 0.0 0.0 -90.55; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z ---------- sensor 2-4 ----------- + hydro water_surface 0.0 0.0 ; x,y gl. pos ---------- sensor 5 ----------- +; general constant 0.0; + dll inpvec 1 9 # Electrical power generator [kW]; ---------- sensor 6 ----------- +; general constant 0.0; + dll inpvec 1 6 # Mgen fast; ---------- sensor 7 ----------- + mbdy state pos blade1 18 1.0 hub1 only 1 # blade 1 tip pos ; ---------- sensor 8-9 ----------- + mbdy state pos blade1 18 1.0 hub1 only 2 # blade 1 tip pos ; ---------- sensor 8-9 ----------- + mbdy state_rot proj_ang blade1 18 1.0 blade1 only 3 # blade 1 tip twist ; ---------- sensor 10 ----------- ???checkes????? +; general constant 0.0; + constraint bearing2 pitch1 5 only 1; Blade1 pitch angle ---------- sensor 11 ----------- +; general constant 0.0; +; general constant 0.0; + constraint bearing1 shaft_rot 2; Azimut Angle and angle velocity ---------- sensor 12-13 ----------- +; general constant 0.0; + dll inpvec 1 5 # Gen speed fast; ---------- sensor 14 ----------- + mbdy state pos towertop 1 1.0 global # tower top position ; ---------- sensor 15-16 ----------- + mbdy state_rot proj_ang towertop 1 1.0 global # tower top twist ; ---------- sensor 17 ----------- + mbdy momentvec blade1 10 1 local # blade 1 50 bending moment% (local e coo) ; ---------- sensor 18-19 ----------- +; mbdy forcevec blade1 1 1 hub1 # blade 1 root shear force and axial force ; ---------- sensor 20-22 ----------- +; mbdy momentvec blade1 1 1 hub1 # blade 1 root bending moment ; ---------- sensor 23-25 ----------- + mbdy forcevec hub1 1 2 hub1 # blade 1 root shear force and axial force ; ---------- sensor 20-22 ----------- + mbdy momentvec hub1 1 2 hub1 # blade 1 root bending moment ; ---------- sensor 23-25 ----------- + mbdy momentvec shaft 4 1 shaft # main bearing ; ---------- sensor 27-28 ----------- + mbdy forcevec towertop 1 1 towertop # tower top shear force ; ---------- sensor 29-31 ----------- + mbdy momentvec towertop 1 1 towertop # tower top bending moment ; ---------- sensor 31-34 ----------- + mbdy state pos tower 1 0.0 global # tower bottom/tp position ; ---------- sensor 35-36 ----------- + mbdy state_rot proj_ang tow_dummy 1 0.0 global # tower bottom/tp twist ; ---------- sensor 37-40 ----------- +; mbdy forcevec L2 8 0.0 L2 # Leg 2 axial force at k-joint position ; ---------- sensor 41 ----------- + mbdy forcevec L2 7 1.0 L2 # Leg 2 axial force at k-joint position ; ---------- sensor 41 ----------- +; mbdy forcevec L4 8 0.0 L4 # Leg 4 axial force at k-joint position ; ---------- sensor 42 ----------- + mbdy forcevec L4 7 1.0 L4 # Leg 4 axial force at k-joint position ; ---------- sensor 42 ----------- + mbdy state pos S2X3A 1 1.0 global # x-2 position side 2 ; ---------- sensor 43 ----------- + mbdy state pos S3X3A 1 1.0 global # x-2 position side 3 ; ---------- sensor 44 ----------- + mbdy state pos S2X1A 3 1.0 global # x-4 position side 2 ; ---------- sensor 45 ----------- måske revideres pga nyt punkt + mbdy state pos S3X1A 3 1.0 global # x-4 position side 3 ; ---------- sensor 46 ----------- + mbdy forcevec S2X1A 3 1 S2X1A # b59 brace position side 2 ; ---------- sensor 47 ----------- nyt punkt ind her til før det passser!!! + mbdy forcevec S2X1A 3 1 global # b59 brace position side 2 ; ---------- sensor 48 ----------- + mbdy forcevec S3X1A 3 1 S3X1A # b61 brace position side 3 ; ---------- sensor 49 ----------- + mbdy forcevec S3X1A 3 1 global # b61 brace position side 3 ; ---------- sensor 50 ----------- + mbdy forcevec L2 2 1.0 L2 only 3 # Leg 2 axial force at mudbrace position ; ---------- sensor 51 ----------- + mbdy forcevec L4 2 1.0 L4 only 3 # Leg 4 axial force at mudbrace position ; ---------- sensor 52 ----------- + mbdy forcevec Pile1 1 1 global # Pile1 shear force ; ---------- sensor 52-54,58 ----------- + mbdy forcevec Pile2 1 1 global # Pile1 shear force ; ---------- sensor 52-54,58 ----------- + mbdy forcevec Pile3 1 1 global # Pile1 shear force ; ---------- sensor 52-54,58 ----------- + mbdy forcevec Pile4 1 1 global # Pile1 shear force ; ---------- sensor 52-54,58 ----------- + mbdy momentvec Pile1 1 1 global # Pile1 moment vector ; ---------- sensor 55-57 ----------- + mbdy momentvec Pile2 1 1 global # Pile1 moment vector ; ---------- sensor 55-57 ----------- + mbdy momentvec Pile3 1 1 global # Pile1 moment vector ; ---------- sensor 55-57 ----------- + mbdy momentvec Pile4 1 1 global # Pile1 moment vector ; ---------- sensor 55-57 ----------- +end output; +exit; + -- GitLab