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bigfootedbigfooted
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update regression restarts
1 parent d0ebabe commit 29b8a6e

12 files changed

Lines changed: 315 additions & 1551 deletions

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‎TestCases/axisymmetric_rans/air_nozzle/air_nozzle.cfg‎

Lines changed: 0 additions & 103 deletions
This file was deleted.

‎TestCases/axisymmetric_rans/air_nozzle/air_nozzle_restart.cfg‎

Lines changed: 2 additions & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -86,15 +86,15 @@ CFL_REDUCTION_TURB= 1.0
8686
%
8787
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
8888
%
89-
ITER= 1000
89+
ITER= 3000
9090
CONV_RESIDUAL_MINVAL= -12
9191
CONV_STARTITER= 10
9292
%
9393
% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
9494
%
9595
MESH_FILENAME= nozzle.su2
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%
97-
SOLUTION_FILENAME= restart_flow.dat
97+
SOLUTION_FILENAME= solution_flow.dat
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RESTART_FILENAME= restart_flow.dat
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OUTPUT_WRT_FREQ= 1000
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%

‎TestCases/hybrid_regression.py‎

Lines changed: 0 additions & 28 deletions
Original file line numberDiff line numberDiff line change
@@ -249,15 +249,6 @@ def main():
249249
### Axisymmetric Compressible RANS ###
250250
#######################################
251251

252-
# Axisymmetric air nozzle (transonic)
253-
axi_rans_air_nozzle = TestCase('axi_rans_air_nozzle')
254-
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
255-
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
256-
axi_rans_air_nozzle.test_iter = 50
257-
axi_rans_air_nozzle.test_vals = [-3.896930, 1.677006, 0.241104, 4.719832, -303.650000]
258-
axi_rans_air_nozzle.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130, -1938.200000]
259-
test_list.append(axi_rans_air_nozzle)
260-
261252
# Axisymmetric air nozzle (transonic)
262253
axi_rans_air_nozzle_restart = TestCase('axi_rans_air_nozzle_restart')
263254
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
@@ -543,15 +534,6 @@ def main():
543534
### Turbomachinery ###
544535
######################################
545536

546-
# Jones APU Turbocharger
547-
Jones_tc = TestCase('jones_turbocharger')
548-
Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"
549-
Jones_tc.cfg_file = "Jones.cfg"
550-
Jones_tc.test_iter = 5
551-
Jones_tc.test_vals = [-5.283765, 0.374023, 72.237490, 1.276352]
552-
Jones_tc.new_output = False
553-
test_list.append(Jones_tc)
554-
555537
# Jones APU Turbocharger restart
556538
Jones_tc_restart = TestCase('jones_turbocharger_restart')
557539
Jones_tc_restart.cfg_dir = "turbomachinery/APU_turbocharger"
@@ -571,16 +553,6 @@ def main():
571553
axial_stage2D.new_output = False
572554
test_list.append(axial_stage2D)
573555

574-
# 2D transonic stator
575-
transonic_stator = TestCase('transonic_stator')
576-
transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"
577-
transonic_stator.cfg_file = "transonic_stator.cfg"
578-
transonic_stator.test_iter = 20
579-
transonic_stator.test_vals = [-0.556926, 5.833298, 96.475820, 0.062519]
580-
transonic_stator.test_vals_aarch64 = [-0.565610, 5.833410, 96.476160, 0.062517]
581-
transonic_stator.new_output = False
582-
test_list.append(transonic_stator)
583-
584556
# 2D transonic stator restart
585557
transonic_stator_restart = TestCase('transonic_stator_restart')
586558
transonic_stator_restart.cfg_dir = "turbomachinery/transonic_stator_2D"

‎TestCases/parallel_regression.py‎

Lines changed: 0 additions & 27 deletions
Original file line numberDiff line numberDiff line change
@@ -389,15 +389,6 @@ def main():
389389
### Axisymmetric Compressible RANS ###
390390
#######################################
391391

392-
# Axisymmetric air nozzle (transonic)
393-
axi_rans_air_nozzle = TestCase('axi_rans_air_nozzle')
394-
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
395-
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
396-
axi_rans_air_nozzle.test_iter = 10
397-
axi_rans_air_nozzle.test_vals = [-1.619755, 3.971206, -7.170784, 4.821522, 66.092000]
398-
axi_rans_air_nozzle.tol = 0.0001
399-
test_list.append(axi_rans_air_nozzle)
400-
401392
# Axisymmetric air nozzle (transonic) restart
402393
axi_rans_air_nozzle_restart = TestCase('axi_rans_air_nozzle_restart')
403394
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
@@ -927,15 +918,6 @@ def main():
927918
### Turbomachinery ###
928919
######################################
929920

930-
# Jones APU Turbocharger
931-
Jones_tc = TestCase('jones_turbocharger')
932-
Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"
933-
Jones_tc.cfg_file = "Jones.cfg"
934-
Jones_tc.test_iter = 5
935-
Jones_tc.test_vals = [-5.283772, 0.374024, 72.236800, 1.276420]
936-
Jones_tc.new_output = False
937-
test_list.append(Jones_tc)
938-
939921
# Jones APU Turbocharger restart
940922
Jones_tc_restart = TestCase('jones_turbocharger_restart')
941923
Jones_tc_restart.cfg_dir = "turbomachinery/APU_turbocharger"
@@ -954,15 +936,6 @@ def main():
954936
axial_stage2D.new_output = False
955937
test_list.append(axial_stage2D)
956938

957-
# 2D transonic stator
958-
transonic_stator = TestCase('transonic_stator')
959-
transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"
960-
transonic_stator.cfg_file = "transonic_stator.cfg"
961-
transonic_stator.test_iter = 20
962-
transonic_stator.test_vals = [-0.571225, 5.831323, 96.911330, 0.062993]
963-
transonic_stator.new_output = False
964-
test_list.append(transonic_stator)
965-
966939
# 2D transonic stator restart
967940
transonic_stator_restart = TestCase('transonic_stator_restart')
968941
transonic_stator_restart.cfg_dir = "turbomachinery/transonic_stator_2D"

‎TestCases/serial_regression.py‎

Lines changed: 2 additions & 29 deletions
Original file line numberDiff line numberDiff line change
@@ -348,15 +348,6 @@ def main():
348348
### Axisymmetric Compressible RANS ###
349349
#######################################
350350

351-
# Axisymmetric air nozzle (transonic) start
352-
axi_rans_air_nozzle = TestCase('axi_rans_air_nozzle')
353-
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
354-
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
355-
axi_rans_air_nozzle.test_iter = 20
356-
axi_rans_air_nozzle.test_vals = [-2.614180, 3.073672, -6.599457, 4.471847, 193.720000]
357-
axi_rans_air_nozzle.tol = 0.0001
358-
test_list.append(axi_rans_air_nozzle)
359-
360351
# Axisymmetric air nozzle (transonic) restart
361352
axi_rans_air_nozzle_restart = TestCase('axi_rans_air_nozzle_restart')
362353
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
@@ -922,19 +913,10 @@ def main():
922913
### turbomachinery ###
923914
######################################
924915

925-
# Jones APU Turbocharger
926-
Jones_tc = TestCase('jones_turbocharger')
927-
Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"
928-
Jones_tc.cfg_file = "Jones.cfg"
929-
Jones_tc.test_iter = 5
930-
Jones_tc.test_vals = [-5.283772, 0.374025, 72.237120, 1.276385] #last 4 columns
931-
Jones_tc.new_output = False
932-
test_list.append(Jones_tc)
933-
934916
# Jones APU Turbocharger restart
935917
Jones_tc_restart = TestCase('jones_turbocharger_restart')
936918
Jones_tc_restart.cfg_dir = "turbomachinery/APU_turbocharger"
937-
Jones_tc_restart.cfg_file = "Jones_rst.cfg"
919+
Jones_tc_restart.cfg_file = "Jones_restart.cfg"
938920
Jones_tc_restart.test_iter = 5
939921
Jones_tc_restart.test_vals = [-4.239857, -1.473748, 33.995240, 10.181660] #last 4 columns
940922
Jones_tc_restart.new_output = False
@@ -950,19 +932,10 @@ def main():
950932
axial_stage2D.new_output = False
951933
test_list.append(axial_stage2D)
952934

953-
# 2D transonic stator
954-
transonic_stator = TestCase('transonic_stator')
955-
transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"
956-
transonic_stator.cfg_file = "transonic_stator.cfg"
957-
transonic_stator.test_iter = 20
958-
transonic_stator.test_vals = [-0.555500, 5.833435, 96.257430, 0.062600] #last 4 columns
959-
transonic_stator.new_output = False
960-
test_list.append(transonic_stator)
961-
962935
# 2D transonic stator restart
963936
transonic_stator_restart = TestCase('transonic_stator_restart')
964937
transonic_stator_restart.cfg_dir = "turbomachinery/transonic_stator_2D"
965-
transonic_stator_restart.cfg_file = "transonic_stator_rst.cfg"
938+
transonic_stator_restart.cfg_file = "transonic_stator_restart.cfg"
966939
transonic_stator_restart.test_iter = 20
967940
transonic_stator_restart.test_vals = [-3.309645, 0.206411, 5.003080, 0.002950] #last 4 columns
968941
transonic_stator_restart.new_output = False

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