Skip to content

Commit e881a6c

Browse files
author
rois1995
committed
- Add regression test case
1 parent fa412f8 commit e881a6c

6 files changed

Lines changed: 30 additions & 16 deletions

‎TestCases/parallel_regression.py‎

Lines changed: 8 additions & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -646,6 +646,14 @@ def main():
646646
schubauer_klebanoff_transition.test_vals = [-7.994740, -13.240225, 0.000046, 0.007987]
647647
test_list.append(schubauer_klebanoff_transition)
648648

649+
# Eppler E387 Transition Case
650+
eppler_e387_transition = TestCase('Eppler_E387')
651+
eppler_e387_transition.cfg_dir = "transition/E387_Airfoil"
652+
eppler_e387_transition.cfg_file = "transitional_SA_LM_model_ConfigFile.cfg"
653+
eppler_e387_transition.test_iter = 10
654+
eppler_e387_transition.test_vals = [-6.674782, -4.987298, -1.544803, 2.297538, 1.542486, 2, -9.258345]
655+
test_list.append(eppler_e387_transition)
656+
649657
#####################################
650658
### Cont. adj. compressible Euler ###
651659
#####################################

‎TestCases/serial_regression.py‎

Lines changed: 8 additions & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -593,6 +593,14 @@ def main():
593593
schubauer_klebanoff_transition.test_vals = [-8.029786, -13.240213, 0.000053, 0.007986] #last 4 columns
594594
test_list.append(schubauer_klebanoff_transition)
595595

596+
# Eppler E387 Transition Case
597+
eppler_e387_transition = TestCase('Eppler_E387')
598+
eppler_e387_transition.cfg_dir = "transition/E387_Airfoil"
599+
eppler_e387_transition.cfg_file = "transitional_SA_LM_model_ConfigFile.cfg"
600+
eppler_e387_transition.test_iter = 10
601+
eppler_e387_transition.test_vals = [-6.665097, -4.986983, -1.559560, 2.355792, 1.563815, 3, -7.644175]
602+
test_list.append(eppler_e387_transition)
603+
596604
#####################################
597605
### Cont. adj. compressible Euler ###
598606
#####################################

‎TestCases/transition/E387_Airfoil/transitional_SA_LM_model_ConfigFile.cfg‎

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -146,6 +146,6 @@ OUTPUT_WRT_FREQ= 500
146146
%
147147
SCREEN_WRT_FREQ_INNER= 10
148148
%
149-
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_INTERMITTENCY, RMS_RE_THETA_T, LIFT, DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS, MAX_DENSITY, MAX_INTERMITTENCY, MAX_RE_THETA_T)
149+
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_INTERMITTENCY, RMS_RE_THETA_T, LIFT, DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS)
150150
%
151151
WRT_PERFORMANCE = YES

‎TestCases/transition/E387_Airfoil/transitional_SST_LM_model_ConfigFile.cfg‎

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -145,6 +145,6 @@ OUTPUT_WRT_FREQ= 500
145145
%
146146
SCREEN_WRT_FREQ_INNER= 10
147147
%
148-
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_INTERMITTENCY, RMS_RE_THETA_T, LIFT, DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS, MAX_INTERMITTENCY, MAX_RE_THETA_T)
148+
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_INTERMITTENCY, RMS_RE_THETA_T, LIFT, DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS)
149149
%
150150
WRT_PERFORMANCE = YES

‎TestCases/transition/Prolate_Spheroid/transitional_SA_LM_model_ConfigFile.cfg‎

Lines changed: 6 additions & 7 deletions
Original file line numberDiff line numberDiff line change
@@ -1,12 +1,11 @@
11
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
22
% %
33
% SU2 configuration file %
4-
% Case description: 2D NACA 0012 Airfoil Validation Case (compressible) %
5-
% http://turbmodels.larc.nasa.gov/naca0012_val_sa.html %
6-
% Author: Francisco Palacios %
7-
% Institution: Stanford University %
8-
% Date: Feb 18th, 2013 %
9-
% File Version 3.2.1 "eagle" %
4+
% Case description: Prolate Spheroid at 15deg %
5+
% Author: Andrea Rausa %
6+
% Institution: Politecnico di Milano %
7+
% Date: Dec 07th, 2022 %
8+
% File Version 7.5.0 "Blackbird" %
109
% %
1110
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
1211

@@ -160,6 +159,6 @@ OUTPUT_WRT_FREQ= 500
160159
%
161160
SCREEN_WRT_FREQ_INNER= 10
162161
%
163-
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_VELOCITY-Z, RMS_TKE, RMS_NU_TILDE, RMS_RE_THETA_T, LIFT, DRAG, CAUCHY_LIFT, CAUCHY_DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS, MAX_PRESSURE, MAX_VELOCITY-X, MAX_VELOCITY-Y, MAX_VELOCITY-Z, MAX_NU_TILDE, MAX_INTERMITTENCY, MAX_RE_THETA_T)
162+
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_NU_TILDE, RMS_RE_THETA_T, LIFT, DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS)
164163
%
165164
WRT_PERFORMANCE = YES

‎TestCases/transition/Prolate_Spheroid/transitional_SST_LM2015_model_ConfigFile.cfg‎

Lines changed: 6 additions & 7 deletions
Original file line numberDiff line numberDiff line change
@@ -1,12 +1,11 @@
11
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
22
% %
33
% SU2 configuration file %
4-
% Case description: 2D NACA 0012 Airfoil Validation Case (compressible) %
5-
% http://turbmodels.larc.nasa.gov/naca0012_val_sa.html %
6-
% Author: Francisco Palacios %
7-
% Institution: Stanford University %
8-
% Date: Feb 18th, 2013 %
9-
% File Version 3.2.1 "eagle" %
4+
% Case description: Prolate Spheroid at 15deg %
5+
% Author: Andrea Rausa %
6+
% Institution: Politecnico di Milano %
7+
% Date: Dec 07th, 2022 %
8+
% File Version 7.5.0 "Blackbird" %
109
% %
1110
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
1211

@@ -162,6 +161,6 @@ OUTPUT_WRT_FREQ= 500
162161
%
163162
SCREEN_WRT_FREQ_INNER= 10
164163
%
165-
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_VELOCITY-Z, RMS_TKE, RMS_DISSIPATION, RMS_INTERMITTENCY, RMS_RE_THETA_T, LIFT, DRAG, CAUCHY_LIFT, CAUCHY_DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS, MAX_PRESSURE, MAX_VELOCITY-X, MAX_VELOCITY-Y, MAX_VELOCITY-Z, MAX_TKE, MAX_DISSIPATION, MAX_INTERMITTENCY, MAX_RE_THETA_T, MAX_CFL, ùAVG_CFL, MIN_CFL)
164+
SCREEN_OUTPUT=(INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_NU_TILDE, RMS_RE_THETA_T, LIFT, DRAG, LINSOL_ITER_TRANS, LINSOL_RESIDUAL_TRANS)
166165
%
167166
WRT_PERFORMANCE = YES

0 commit comments

Comments
 (0)