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Commit db319c73 authored by Mads M. Pedersen's avatar Mads M. Pedersen
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improved auto_detect_modelpath

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wetb/hawc2/bladeinfo.py
+ 1
− 1
View file @ db319c73
......@@ -93,7 +93,7 @@ class H2BladeInfo(BladeInfo, PCFile, AtTimeFile):
blade_name = blade_name or htcfile.aero.link[2]
s = htcfile.new_htc_structure
at_time_filename = at_time_filename or os.path.join(htcfile.modelpath, htcfile.output_at_time.filename[0] + ".dat")
at_time_filename = at_time_filename or ("output_at_time" in htcfile and os.path.join(htcfile.modelpath, htcfile.output_at_time.filename[0] + ".dat"))
pc_filename = pc_filename or os.path.join(htcfile.modelpath, htcfile.aero.pc_filename[0])
ae_filename = ae_filename or os.path.join(htcfile.modelpath, htcfile.aero.ae_filename[0])
......
wetb/hawc2/htc_file.py
+ 20
− 11
View file @ db319c73
......@@ -87,7 +87,7 @@ class HTCFile(HTCContents, HTCDefaults):
if filename is not None:
self.filename = filename
self.modelpath = modelpath or self.auto_detect_modelpath()
if filename and not os.path.isabs(self.modelpath):
if filename and self.modelpath!="unknown" and not os.path.isabs(self.modelpath):
self.modelpath = os.path.realpath(os.path.join(os.path.dirname(self.filename), self.modelpath))
......@@ -99,11 +99,14 @@ class HTCFile(HTCContents, HTCDefaults):
#print (["../"*i for i in range(3)])
import numpy as np
found = ([np.sum([os.path.isfile(os.path.join(os.path.dirname(self.filename), "../"*i, f)) for f in self.input_files() if not os.path.isabs(f)]) for i in range(4)])
input_files = HTCFile(self.filename, 'unknown').input_files()
rel_input_files = [f for f in input_files if not os.path.isabs(f)]
found = ([np.sum([os.path.isfile(os.path.join(os.path.dirname(self.filename), "../"*i, f)) for f in rel_input_files]) for i in range(4)])
#for f in self.input_files():
# print (os.path.isfile(os.path.join(os.path.dirname(self.filename), "../",f)), f)
if max(found)>0:
return "../"* np.argmax(found)
relpath = "../"* np.argmax(found)
return os.path.abspath(os.path.join(os.path.dirname(self.filename), relpath))
else:
raise ValueError("Modelpath cannot be autodetected for '%s'.\nInput files not found near htc file"%self.filename)
......@@ -161,12 +164,15 @@ class HTCFile(HTCContents, HTCDefaults):
for l in lines:
if l.lower().lstrip().startswith('continue_in_file'):
filename = l.lstrip().split(";")[0][len("continue_in_file"):].strip().lower()
filename = os.path.join(self.modelpath, filename)
for line in self.readlines(filename):
if line.lstrip().lower().startswith('exit'):
break
htc_lines.append(line)
if self.modelpath=='unknown':
self.htc_inputfiles.append(filename)
else:
filename = os.path.join(self.modelpath, filename)
for line in self.readlines(filename):
if line.lstrip().lower().startswith('exit'):
break
htc_lines.append(line)
else:
htc_lines.append(l)
return htc_lines
......@@ -213,12 +219,15 @@ class HTCFile(HTCContents, HTCDefaults):
self.simulation.newmark.deltat = step
if start is not None:
self.output.time = start, stop
if "wind" in self and self.wind.turb_format[0] > 0:
if "wind" in self:# and self.wind.turb_format[0] > 0:
self.wind.scale_time_start = start
def input_files(self):
self.contents # load if not loaded
files = [os.path.abspath(f).replace("\\","/") for f in self.htc_inputfiles]
if self.modelpath=="unknown":
files = [f.replace("\\","/") for f in self.htc_inputfiles]
else:
files = [os.path.abspath(f).replace("\\","/") for f in self.htc_inputfiles]
if 'new_htc_structure' in self:
for mb in [self.new_htc_structure[mb] for mb in self.new_htc_structure.keys() if mb.startswith('main_body')]:
if "timoschenko_input" in mb:
......
wetb/hawc2/tests/test_files/htcfiles/sub/continue_in_file.htc 0 → 100644
+ 519
− 0
View file @ db319c73
begin Simulation; test
time_stop 10 ;
solvertype 1 ; (newmark)
on_no_convergence continue ;
convergence_limits 1E3 1.0 1E-7 ;
logfile ./log/oc4_p2_Load_case_3-1.log ;
animation ./anim/oc4_p2_Load_case_3-1.dat;
;
begin newmark;
deltat 0.025;
end newmark;
end simulation;
;
begin new_htc_structure;
; beam_output_file_name ./log/oc4_p2_Load_case_3-1_beam.dat; Optional - Calculated beam properties of the bodies are written to file
; body_output_file_name ./log/oc4_p2_Load_case_3-1_body.dat; Optional - Body initial position and orientation are written to file
; struct_inertia_output_file_name ./log/oc4_p2_Load_case_3-1_struct.dat;
; body_eigenanalysis_file_name ./oc4_load_case_1_1/oc4_p2_Load_case_3-1_body_eigen.dat;
; structure_eigenanalysis_file_name ./oc4_load_case_1_1/oc4_p2_Load_case_3-1_strc_eigen.dat ;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
;
continue_in_file OC5_Phase_II.mbdy; Definition of substructure
;
begin main_body;
name tower ;
type timoschenko ;
nbodies 1 ;
node_distribution c2_def;
; concentrated_mass 1 0.0 0.0 0.0 125332 0.0 0.0 0.0 ; un-tuned values instrument mass 101762.00
concentrated_mass 1 0.0 0.0 0.0 87846 0.0 0.0 0.0 ; tuned values instrument mass
damping_posdef 0.0 0.0 0.0 0.86E-02 0.87E-02 4.3E-03 ;
gravity 9.80665;
begin timoschenko_input ;
filename ./data/OC5_5MW_st.txt ;
set 1 2 ; set subset
end timoschenko_input;
begin c2_def; Definition of centerline (main_body coordinates)
nsec 18 ;
sec 1 0 0 0 0 ;
sec 2 0 0 -0.312018 0 ;
sec 3 0 0 -0.313582 0 ;
sec 4 0 0 -8.601218 0 ;
sec 5 0 0 -8.602782 0 ;
sec 6 0 0 -11.651018 0 ;
sec 7 0 0 -11.652582 0 ;
sec 8 0 0 -12.354818 0 ;
sec 9 0 0 -12.356382 0 ;
sec 10 0 0 -72.177818 0 ;
sec 11 0 0 -72.179382 0 ;
sec 12 0 0 -73.429018 0 ;
sec 13 0 0 -73.430582 0 ;
sec 14 0 0 -74.054618 0 ;
sec 15 0 0 -74.056182 0 ;
sec 16 0 0 -74.993018 0 ;
sec 17 0 0 -74.994582 0 ;
sec 18 0 0 -78.2 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 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
; gravity 9.80665;
; begin timoschenko_input;
; filename ./data/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 MC_dummy ; Dummy structure with other element coordinate than the tower, for output only
; type timoschenko ;
; nbodies 1 ;
; node_distribution c2_def ;
; damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
; gravity 9.80665;
; begin timoschenko_input;
; filename ./data/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 9.025E-06 9.025E-06 8.0E-05 8.3E-06 8.3E-06 8.5E-05 ;
damping_posdef 2.50E-04 1.40E-04 2.00E-03 3.00E-05 3.00E-05 2.00E-04 ;
concentrated_mass 1 0.0 -1.13 0.0 4.7790E+05 8.5004E+07 6.6413E+07 8.4394E+07; Nacelle mass and inertia
gravity 9.80665;
begin timoschenko_input;
filename ./data/NREL_5MW_st.txt ;
set 2 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 -1.8 0.0 ;
end c2_def ;
end main_body;
;
begin main_body;
name shaft ;
type timoschenko ;
nbodies 1 ;
node_distribution c2_def ;
; damping_posdef 7.00E-3 7.00E-03 7.00E-02 3.48E-04 3.48E-04 1.156E-03 ;
damping_posdef 0.0 0.0 7.0725E-03 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"
gravity 9.80665;
begin timoschenko_input;
filename ./data/NREL_5MW_st.txt ;
set 3 2 ;
end timoschenko_input;
begin c2_def; Definition of centerline (main_body coordinates)
nsec 5;
sec 1 0.0 0.0 0.0 0.0 ; Tower top x,y,z,twist
sec 2 0.0 0.0 1.0 0.0 ;
sec 3 0.0 0.0 2.0 0.0 ;
sec 4 0.0 0.0 5.0 0.0 ; Main bearing
sec 5 0.0 0.0 10.6 0.0 ; Rotor centre
end c2_def ;
end main_body;
;
begin main_body;
name hub1 ;
type timoschenko ;
nbodies 1 ;
node_distribution c2_def ;
damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
gravity 9.80665;
begin timoschenko_input;
filename ./data/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 1 ;
node_distribution c2_def;
concentrated_mass 7 0.0 0.0 2.004 2.2333E+4 0.0 0.0 0.0 ; Blade mass
concentrated_mass 1 0.0 0.0 0.0 0.0 5.46E+06 5.46E+06 0.0 ; Blade additional inertia
damping_posdef 0.0 0.0 0.0 1.41E-03 2.39E-03 4.5E-05 ; Mx My Mz Kx Ky Kz , M? raises overall level, K? raises high freguency level (3% log.decr with 9 bodies
begin timoschenko_input ;
filename ./data/OC5_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 0 0 -50.377 ; x.y.z. twist
sec 2 0 0 1.398 -42.712 ;
sec 3 0 0 4.107 -31.187 ;
sec 4 0 0 6.816 -23.109 ;
sec 5 0 0 10.281 -16.389 ;
sec 6 0 0 14.376 -11.475 ;
sec 7 0 0 18.471 -8.502 ;
sec 8 0 0 22.566 -6.523 ;
sec 9 0 0 26.661 -5.052 ;
sec 10 0 0 30.756 -3.878 ; 50% blade radius
sec 11 0 0 34.851 -2.939 ;
sec 12 0 0 38.946 -2.216 ;
sec 13 0 0 43.041 -1.673 ;
sec 14 0 0 47.136 -1.245 ;
sec 15 0 0 51.231 -0.844 ;
sec 16 0 0 54.696 -0.497 ;
sec 17 0 0 57.405 -0.235 ;
sec 18 0 0 60.114 -0.064 ;
sec 19 0 0 61.5 0.0 ;
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;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
; continue_in_file ./mooring_dynamic_init.inc ;
; continue_in_file ./mooring_dynamic.inc;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
begin orientation;
;----------------------------
continue_in_file ./orientation.dat;
;----------------------------
;
begin base;
body tower;
inipos 0.0 0.0 0.0 ; initial position of node 1
body_eulerang 0.0 0.0 0.0;
end base;
;
; begin relative;
; body1 MC last;
; body2 tower 1;
; body2_eulerang 0.0 0.0 0.0;
; end relative;
; ;
; begin relative;
; body1 MC 8;
; body2 MC_dummy 1;
; body2_eulerang 0.0 0.0 0.0;
; end relative;
;
; 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 1;
body2_eulerang 90.0 0.0 0.0;
body2_eulerang 0.0 0.0 0.0; 0 deg tilt angle
; body2_ini_rotvec_d1 0.0 0.0 -1.0 0.942477795 ; 12.1 rpm body initial rotation velocity x.y.z.angle velocity[rad/s] (body 2 coordinates)
end relative;
;
begin relative;
body1 shaft last;
body2 hub1 1;
body2_eulerang -90.0 0.0 0.0;
body2_eulerang 0.0 180.0 0.0;
body2_eulerang 0.0 0.0 0.0; 0deg cone angle
end relative;
;
begin relative;
body1 shaft last;
body2 hub2 1;
body2_eulerang -90.0 0.0 0.0;
body2_eulerang 0.0 60.0 0.0;
body2_eulerang 0.0 0.0 0.0; 0eg cone angle
end relative;
;
begin relative;
body1 shaft last;
body2 hub3 1;
body2_eulerang -90.0 0.0 0.0;
body2_eulerang 0.0 -60.0 0.0;
body2_eulerang 0.0 0.0 0.0; 0deg 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 ./constraint.dat;
;---------------------------
;
; begin fix0;
; mbdy tower;
; ; disable_at ;
; end fix0;
;
;--------------------------- constraints Turbine
;
begin fix1;
mbdy1 MC last;
mbdy2 tower 1;
end fix1;
;
; begin fix1;
; mbdy1 tower 1;
; mbdy2 tow_dummy 1;
; end fix1;
;
; begin fix1;
; mbdy1 MC 8;
; mbdy2 MC_dummy 1;
; end fix1;
;
begin fix1;
body1 tower last ;
body2 towertop 1;
end fix1;
;
; begin bearing1; free bearing
; name shaft_rot;
; body1 towertop last;
; body2 shaft 1;
; 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; fixed rotor
body1 towertop last ;
body2 shaft 1;
end fix1;
;
begin fix1;
body1 shaft last ;
body2 hub1 1;
end fix1;
;
begin fix1;
body1 shaft last ;
body2 hub2 1;
end fix1;
;
begin fix1;
body1 shaft last ;
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;
;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
; continue_in_file ./mooring_constraints.inc ;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
end constraint;
;
end new_htc_structure;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------begin hydro;
begin hydro;
begin water_properties;
rho 1025;
wave_direction 0 ;
gravity 9.80665;
; current 2 0.5 0.1429 0; type, vel, alpha, current direction.
mwl 0.00;
mudlevel 200;
; water_kinematics_dll ./wkin_dll.dll ./htc_hydro/reg_airy_h6_t10.inp;
end water_properties;
;-------------------------------------------------------------
; continue_in_file OC4_Phase_II_nw.hydro;
continue_in_file OC5_Phase_II.hydro;
;-------------------------------------------------------------
end hydro;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
; begin wind ;
; density 1.225 ; to be checked
; wsp 8 ;
; tint 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 -90.0 ;
; shear_format 1 0 ;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 350 ;
; ;
; ; begin mann;
; ; filename_u ./turb/u.bin ;
; ; filename_v ./turb/v.bin ;
; ; filename_w ./turb/w.bin ;
; ; box_dim_u 32768 ; ;
; ; box_dim_v 64 3.125000119E+00;
; ; box_dim_w 32 4.679999948E+00;
; ; std_scaling 1.0 0.8 0.502 ;
; ; end mann;
; ;
; begin tower_shadow_potential_2;
; tower_mbdy_link tower;
; nsec 4;
; radius 0.0 1.683 ;
; radius 12.09 1.683 ;
; radius 12.1 1.27 ;
; radius 78.2 1.27 ;
; end tower_shadow_potential_2;
; 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/OC5_5MW_ae.txt;
; pc_filename ./data/OC5_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 ??method,2=mhh method
; end aero ;
;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
;
;----------------------------------------------------------------------------------------------------------------------------------------------------------------
begin output;
filename ./res/oc4_p2_Load_case_eq ;
;
; data_format hawc_ascii;
; time 350 410 ;
buffer 1 ;
;
general time;---------- sensor 1 -----------
; wind free_wind 1 0.0 0.0 -90.0; 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 ; sensor 6 - electrical power kW
; general constant 0.0 ; sensor 7 - electrical generator torque kNm
; general constant 0.0;Azimut Angle and angle velocity ---------- sensor 8-9
; general constant 0.0;Azimut Angle and angle velocity ---------- sensor 8-9
; constraint bearing1 shaft_rot 2; Azimut Angle and angle velocity ---------- sensor 8-9 -----------
; general constant 0.0; generator high speed rpm
mbdy state pos blade1 18 1.0 hub1 only 2 # blade 1 tip pos ; ---------- sensor 11-12 -----------
mbdy state pos blade1 18 1.0 hub1 only 1 # blade 1 tip pos ; ---------- sensor 11-12 -----------
mbdy state_rot proj_ang blade1 18 1.0 blade1 only 3 # blade 1 tip twist ; ---------- sensor 13 -----------
; constraint bearing2 pitch1 5 only 1; Blade1 pitch angle ---------- sensor 14 -----------
; mbdy state pos towertop 1 1.0 tow_dummy # tower top flange position ; ---------- sensor 15-17-----------
; mbdy state_rot proj_ang towertop 1 1.0 tow_dummy only 3 tower top twist ; ---------- sensor 13 -----------
;
; mbdy state pos MC 8 0.0 global # platform translation in surge sway and heave ; ---------- sensor 18-20-----------
; mbdy state_rot proj_ang MC_dummy 1 0.0 global # platform rotation in roll pitch and yaw ; ---------- sensor 21-23 -----------
;
mbdy forcevec hub1 1 2 hub1 # blade 1 root shear force and axial force ; ---------- sensor 24-26 -----------
mbdy momentvec hub1 1 2 hub1 # blade 1 root bending moment ; ---------- sensor 27-29 -----------
mbdy momentvec shaft 4 1 shaft # main bearing ; ---------- sensor 30-32 -----------
mbdy forcevec towertop 1 1 towertop # tower top shear force ; ---------- sensor 33-35 -----------
mbdy momentvec towertop 1 1 towertop # tower top bending moment ; ---------- sensor 36-38 -----------
mbdy forcevec tower 1 1 tower # tower base shear force ; ---------- sensor 39-41 -----------
mbdy momentvec tower 1 1 tower # tower base bending moment ; ---------- sensor 42-44 -----------
; mbdy forcevec YU1 3 2 YU1 # tower base shear force ; ---------- sensor 45-47 -----------
; mbdy forcevec DU1 1 2 DU1 # tower base shear force ; ---------- sensor 47-50 -----------
;sensor 51-60 are mooring sensors
; esys line1_1;
; esys line1_3;
; esys line2_1;
; esys line2_3;
; esys line3_1;
; esys line3_3;
end output;
exit;
wetb/hawc2/tests/test_htc_file.py
+ 9
− 0
View file @ db319c73
......@@ -245,6 +245,15 @@ class TestHtcFile(unittest.TestCase):
self.assertEqual(str(htcfile).count("exit"), 1)
self.assertIn('filename\t./res/oc4_p2_load_case_eq;', str(htcfile))
def test_continue_in_files_autodetect_path(self):
htcfile = HTCFile(self.testfilepath + "sub/continue_in_file.htc")
self.assertIn('main_body__31', htcfile.new_htc_structure.keys())
self.assertIn(os.path.abspath(self.testfilepath + 'orientation.dat'), [os.path.abspath(f) for f in htcfile.input_files()])
self.assertIn('./data/NREL_5MW_st1.txt', htcfile.input_files())
self.assertEqual(str(htcfile).count("exit"), 1)
self.assertIn('filename\t./res/oc4_p2_load_case_eq;', str(htcfile))
def test_tjul_example(self):
htcfile = HTCFile(self.testfilepath + "./tjul.htc", ".")
htcfile.save("./temp.htc")
......
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