The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 2,079 KB.. Full Log+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==367190== Memcheck, a memory error detector ==367190== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==367190== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==367190== Command: python tess_6_TriQuad.py ==367190== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 8302 Number of elements = 17191 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 17191 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 8302 Total number of elements = 17191 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 72029 Number of elements = 74322 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 74322 ---------------------------- Total number of nodes = 72029 Total number of elements = 74322 ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1655 Number of elements = 3225 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3225 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1655 Total number of elements = 3225 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 3009 Number of elements = 2928 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 2928 ---------------------------- Total number of nodes = 3009 Total number of elements = 2928 ==367190== ==367190== HEAP SUMMARY: ==367190== in use at exit: 4,094,389 bytes in 24,490 blocks ==367190== total heap usage: 34,013,434 allocs, 33,988,944 frees, 10,567,825,889 bytes allocated ==367190== ==367190== LEAK SUMMARY: ==367190== definitely lost: 0 bytes in 0 blocks ==367190== indirectly lost: 0 bytes in 0 blocks ==367190== possibly lost: 0 bytes in 0 blocks ==367190== still reachable: 0 bytes in 0 blocks ==367190== suppressed: 4,094,389 bytes in 24,490 blocks ==367190== ==367190== For lists of detected and suppressed errors, rerun with: -s ==367190== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1876 from 1876) 686.43user 4.12system 11:33.13elapsed 99%CPU (0avgtext+0avgdata 582300maxresident)k 42792inputs+104280outputs (32major+2674067minor)pagefaults 0swaps real 11m33.139s user 11m26.432s sys 0m4.129s + status=0 + set +x ================================================= data/session09/tess_6_TriQuad.py passed (as expected) ================================================= ================================================= tess_7_MeshSizing.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python tess_7_MeshSizing.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==563922== Memcheck, a memory error detector ==563922== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==563922== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==563922== Command: python tess_7_MeshSizing.py ==563922== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 8302 Number of elements = 17191 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 17191 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 8302 Total number of elements = 17191 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - leadingEdge Mesh sizing name - rootLeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 3919 Number of elements = 8410 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 8410 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3919 Total number of elements = 8410 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting mesh sizing parameters Mesh sizing name - leadingEdge Mesh sizing name - rootLeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 6181 Number of elements = 6607 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6607 ---------------------------- Total number of nodes = 6181 Total number of elements = 6607 ==563922== ==563922== HEAP SUMMARY: ==563922== in use at exit: 4,094,761 bytes in 24,495 blocks ==563922== total heap usage: 21,535,346 allocs, 21,510,851 frees, 6,642,708,154 bytes allocated ==563922== ==563922== LEAK SUMMARY: ==563922== definitely lost: 0 bytes in 0 blocks ==563922== indirectly lost: 0 bytes in 0 blocks ==563922== possibly lost: 0 bytes in 0 blocks ==563922== still reachable: 0 bytes in 0 blocks ==563922== suppressed: 4,094,761 bytes in 24,495 blocks ==563922== ==563922== For lists of detected and suppressed errors, rerun with: -s ==563922== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1878 from 1878) 471.48user 2.42system 7:53.78elapsed 100%CPU (0avgtext+0avgdata 539788maxresident)k 8inputs+41056outputs (0major+1469399minor)pagefaults 0swaps real 7m53.786s user 7m51.484s sys 0m2.433s + status=0 + set +x ================================================= data/session09/tess_7_MeshSizing.py passed (as expected) ================================================= ================================================= tess_8_MeshSizing.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python tess_8_MeshSizing.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==567981== Memcheck, a memory error detector ==567981== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==567981== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==567981== Command: python tess_8_MeshSizing.py ==567981== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1655 Number of elements = 3225 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3225 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1655 Total number of elements = 3225 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - rootLeadingEdge Mesh sizing name - wingSpar1 Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 6587 Number of elements = 13200 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 13200 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 6587 Total number of elements = 13200 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - rootLeadingEdge Mesh sizing name - wingSpar1 Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 22190 Number of elements = 22191 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 22191 ---------------------------- Total number of nodes = 22190 Total number of elements = 22191 ==567981== ==567981== HEAP SUMMARY: ==567981== in use at exit: 4,094,761 bytes in 24,495 blocks ==567981== total heap usage: 23,564,402 allocs, 23,539,907 frees, 6,678,516,824 bytes allocated ==567981== ==567981== LEAK SUMMARY: ==567981== definitely lost: 0 bytes in 0 blocks ==567981== indirectly lost: 0 bytes in 0 blocks ==567981== possibly lost: 0 bytes in 0 blocks ==567981== still reachable: 0 bytes in 0 blocks ==567981== suppressed: 4,094,761 bytes in 24,495 blocks ==567981== ==567981== For lists of detected and suppressed errors, rerun with: -s ==567981== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1878 from 1878) 489.18user 3.15system 8:12.19elapsed 100%CPU (0avgtext+0avgdata 584952maxresident)k 8inputs+43872outputs (0major+1919804minor)pagefaults 0swaps real 8m12.198s user 8m9.184s sys 0m3.157s + status=0 + set +x ================================================= data/session09/tess_8_MeshSizing.py passed (as expected) ================================================= ================================================= tess_MinQuad.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python tess_MinQuad.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==570667== Memcheck, a memory error detector ==570667== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==570667== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==570667== Command: python tess_MinQuad.py ==570667== ==> Loading geometry from file "../../data/ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 299 Number of elements = 387 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 387 ---------------------------- Total number of nodes = 299 Total number of elements = 387 --> Total Elements 387 ==570667== ==570667== HEAP SUMMARY: ==570667== in use at exit: 4,094,133 bytes in 24,490 blocks ==570667== total heap usage: 16,266,241 allocs, 16,241,751 frees, 5,052,877,201 bytes allocated ==570667== ==570667== LEAK SUMMARY: ==570667== definitely lost: 0 bytes in 0 blocks ==570667== indirectly lost: 0 bytes in 0 blocks ==570667== possibly lost: 0 bytes in 0 blocks ==570667== still reachable: 0 bytes in 0 blocks ==570667== suppressed: 4,094,133 bytes in 24,490 blocks ==570667== ==570667== For lists of detected and suppressed errors, rerun with: -s ==570667== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1877 from 1877) 378.72user 1.89system 6:20.52elapsed 100%CPU (0avgtext+0avgdata 534516maxresident)k 272inputs+12664outputs (0major+1006698minor)pagefaults 0swaps real 6m20.529s user 6m18.728s sys 0m1.897s + status=0 + set +x ================================================= solutions/session09/tess_MinQuad.py passed (as expected) ================================================= ================================================= tess_2k.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python tess_2k.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==584604== Memcheck, a memory error detector ==584604== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==584604== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==584604== Command: python tess_2k.py ==584604== ==> Loading geometry from file "../../data/ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - rootLeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1289 Number of elements = 1189 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 1189 ---------------------------- Total number of nodes = 1289 Total number of elements = 1189 --> Total Elements 1189 ==584604== ==584604== HEAP SUMMARY: ==584604== in use at exit: 4,094,612 bytes in 24,493 blocks ==584604== total heap usage: 18,058,210 allocs, 18,033,717 frees, 5,621,502,113 bytes allocated ==584604== ==584604== LEAK SUMMARY: ==584604== definitely lost: 0 bytes in 0 blocks ==584604== indirectly lost: 0 bytes in 0 blocks ==584604== possibly lost: 0 bytes in 0 blocks ==584604== still reachable: 0 bytes in 0 blocks ==584604== suppressed: 4,094,612 bytes in 24,493 blocks ==584604== ==584604== For lists of detected and suppressed errors, rerun with: -s ==584604== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1877 from 1877) 404.40user 1.60system 6:47.77elapsed 99%CPU (0avgtext+0avgdata 546776maxresident)k 8inputs+11360outputs (0major+823451minor)pagefaults 0swaps real 6m47.776s user 6m44.415s sys 0m1.607s + status=0 + set +x ================================================= solutions/session09/tess_2k.py passed (as expected) ================================================= ================================================= astros_1_ModalClamped.py test; + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python astros_1_ModalClamped.py ==605961== Memcheck, a memory error detector ==605961== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==605961== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==605961== Command: python astros_1_ModalClamped.py ==605961== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 ---------------------------- Total number of nodes = 235 Total number of elements = 227 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 --> Eigen-frequencies: 1 : 0.0357647 2 : 0.102451 3 : 0.102451 4 : 0.159637 5 : 0.159637 6 : 0.215446 7 : 0.215446 8 : 0.350115 9 : 0.350115 10: 0.466966 ==605961== ==605961== HEAP SUMMARY: ==605961== in use at exit: 4,096,756 bytes in 24,503 blocks ==605961== total heap usage: 17,768,567 allocs, 17,744,064 frees, 5,597,890,888 bytes allocated ==605961== ==605961== LEAK SUMMARY: ==605961== definitely lost: 0 bytes in 0 blocks ==605961== indirectly lost: 0 bytes in 0 blocks ==605961== possibly lost: 0 bytes in 0 blocks ==605961== still reachable: 0 bytes in 0 blocks ==605961== suppressed: 4,096,756 bytes in 24,503 blocks ==605961== ==605961== For lists of detected and suppressed errors, rerun with: -s ==605961== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1880 from 1880) 429.02user 2.38system 7:17.94elapsed 98%CPU (0avgtext+0avgdata 546792maxresident)k 20216inputs+38624outputs (80major+984770minor)pagefaults 0swaps real 7m17.954s user 7m9.023s sys 0m2.395s + status=0 + set +x ================================================= data/session10/astros_1_ModalClamped.py passed (as expected) ================================================= ================================================= astros_2_ModalSupport.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python astros_2_ModalSupport.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==621078== Memcheck, a memory error detector ==621078== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==621078== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==621078== Command: python astros_2_ModalSupport.py ==621078== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Name = ribSupport, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 Body 2 (of 2) Number of nodes = 1 Number of elements = 1 Number of node elements = 1 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 236 Total number of elements = 228 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = ribRootPoint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = ribRoot, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Name = ribSupport, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 236 Combined Number of elements = 228 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - leftWingSkin Property name - ribSupport Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribRootPoint No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribRootPoint No "groupName" specified for Support tuple ribRootPoint, going to use support name Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - ribRoot No "groupName" specified for Connection tuple ribRoot! Looking for automatic connections from the use of capsConnectLink for ribRoot 19 automatic connections were made for capsConnect ribRoot (node id 236) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing support cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 --> Eigen-frequencies: 1 : 0.0 2 : 0.0357647 3 : 0.0365801 4 : 0.102451 5 : 0.102453 6 : 0.159637 7 : 0.1611 8 : 0.215446 9 : 0.215462 10: 0.350115 ==621078== ==621078== HEAP SUMMARY: ==621078== in use at exit: 4,096,756 bytes in 24,503 blocks ==621078== total heap usage: 17,766,929 allocs, 17,742,426 frees, 5,579,708,702 bytes allocated ==621078== ==621078== LEAK SUMMARY: ==621078== definitely lost: 0 bytes in 0 blocks ==621078== indirectly lost: 0 bytes in 0 blocks ==621078== possibly lost: 0 bytes in 0 blocks ==621078== still reachable: 0 bytes in 0 blocks ==621078== suppressed: 4,096,756 bytes in 24,503 blocks ==621078== ==621078== For lists of detected and suppressed errors, rerun with: -s ==621078== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1880 from 1880) 395.58user 2.19system 6:39.58elapsed 99%CPU (0avgtext+0avgdata 543180maxresident)k 72inputs+40360outputs (2major+942399minor)pagefaults 0swaps real 6m39.587s user 6m35.590s sys 0m2.203s + status=0 + set +x ================================================= data/session10/astros_2_ModalSupport.py passed (as expected) ================================================= ================================================= astros_3_StaticClamped.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python astros_3_StaticClamped.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==652605== Memcheck, a memory error detector ==652605== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==652605== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==652605== Command: python astros_3_StaticClamped.py ==652605== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 ---------------------------- Total number of nodes = 235 Total number of elements = 227 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftPointLoad No "groupName" specified for Load tuple leftPointLoad, going to use load name Load name - ritePointLoad No "groupName" specified for Load tuple ritePointLoad, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... --> Maximum displacements: --> Tmax 43461.879162311016 --> T1max 738.595 --> T2max 3686.25 --> T3max 43363.8 ==652605== ==652605== HEAP SUMMARY: ==652605== in use at exit: 4,096,756 bytes in 24,503 blocks ==652605== total heap usage: 17,777,010 allocs, 17,752,507 frees, 5,605,642,250 bytes allocated ==652605== ==652605== LEAK SUMMARY: ==652605== definitely lost: 0 bytes in 0 blocks ==652605== indirectly lost: 0 bytes in 0 blocks ==652605== possibly lost: 0 bytes in 0 blocks ==652605== still reachable: 0 bytes in 0 blocks ==652605== suppressed: 4,096,756 bytes in 24,503 blocks ==652605== ==652605== For lists of detected and suppressed errors, rerun with: -s ==652605== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1879 from 1879) 397.09user 2.16system 6:39.50elapsed 99%CPU (0avgtext+0avgdata 555456maxresident)k 40inputs+34592outputs (1major+1132963minor)pagefaults 0swaps real 6m39.511s user 6m37.102s sys 0m2.174s + status=0 + set +x ================================================= data/session10/astros_3_StaticClamped.py passed (as expected) ================================================= ================================================= astros_4_Composite.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python astros_4_Composite.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==673426== Memcheck, a memory error detector ==673426== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==673426== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==673426== Command: python astros_4_Composite.py ==673426== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 ---------------------------- Total number of nodes = 235 Total number of elements = 227 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftPointLoad No "groupName" specified for Load tuple leftPointLoad, going to use load name Load name - ritePointLoad No "groupName" specified for Load tuple ritePointLoad, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... --> Maximum displacements: --> Tmax 12131.654370141774 --> T1max 275.241 --> T2max 1005.74 --> T3max 12103.5 ==673426== ==673426== HEAP SUMMARY: ==673426== in use at exit: 4,096,833 bytes in 24,504 blocks ==673426== total heap usage: 17,782,753 allocs, 17,758,249 frees, 5,674,727,627 bytes allocated ==673426== ==673426== LEAK SUMMARY: ==673426== definitely lost: 0 bytes in 0 blocks ==673426== indirectly lost: 0 bytes in 0 blocks ==673426== possibly lost: 0 bytes in 0 blocks ==673426== still reachable: 0 bytes in 0 blocks ==673426== suppressed: 4,096,833 bytes in 24,504 blocks ==673426== ==673426== For lists of detected and suppressed errors, rerun with: -s ==673426== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1879 from 1879) 431.82user 2.98system 7:29.78elapsed 96%CPU (0avgtext+0avgdata 576056maxresident)k 16inputs+34576outputs (0major+1365552minor)pagefaults 0swaps real 7m29.786s user 7m11.831s sys 0m2.992s + status=0 + set +x ================================================= data/session10/astros_4_Composite.py passed (as expected) ================================================= ================================================= nastran_5_Flutter.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python nastran_5_Flutter.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==681707== Memcheck, a memory error detector ==681707== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==681707== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==681707== Command: python nastran_5_Flutter.py ==681707== ==> Loading geometry from file "../ESP/wing3.csm"... Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ==> Running Nastran pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Wing, index = 1 Name = wingSpar2, index = 2 Name = wingRib, index = 3 Name = riteWingSkin, index = 4 Name = wingSpar1, index = 5 Name = leftWingSkin, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 4) Getting surface mesh for body 2 (of 4) Getting surface mesh for body 3 (of 4) Getting surface mesh for body 4 (of 4) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 (of 4) Number of nodes = 11 Number of elements = 6 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 2 (of 4) Number of nodes = 11 Number of elements = 6 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 3 (of 4) Number of nodes = 11 Number of elements = 6 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6 Body 4 (of 4) Number of nodes = 939 Number of elements = 1094 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 1094 ---------------------------- Total number of nodes = 972 Total number of elements = 1112 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Wing, index = 1 Name = wingSpar2, index = 2 Name = wingRib, index = 3 Name = riteWingSkin, index = 4 Name = wingSpar1, index = 5 Name = leftWingSkin, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 11 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 11 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 11 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 939 Number of elements = 1094 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 1094 Combining multiple FEA meshes! Combined Number of nodal coordinates = 972 Combined Number of elements = 1112 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 1112 Getting vortex lattice surface data VLM surface name - upperWing Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 108 Surface 2: Number of points found for aero-spline = 108 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing Nastran instruction file.... Warning: No loads specified for case Flutter!!!! Writing aero card Writing analysis cards Writing constraint ADD cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Writing aeroelastic cards ==> Running Nastran... sh: 1: nastran: not found ==681707== ==681707== HEAP SUMMARY: ==681707== in use at exit: 4,096,391 bytes in 24,499 blocks ==681707== total heap usage: 14,837,345 allocs, 14,812,846 frees, 4,891,332,529 bytes allocated ==681707== ==681707== LEAK SUMMARY: ==681707== definitely lost: 0 bytes in 0 blocks ==681707== indirectly lost: 0 bytes in 0 blocks ==681707== possibly lost: 0 bytes in 0 blocks ==681707== still reachable: 0 bytes in 0 blocks ==681707== suppressed: 4,096,391 bytes in 24,499 blocks ==681707== ==681707== For lists of detected and suppressed errors, rerun with: -s ==681707== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1878 from 1878) 352.30user 2.02system 5:58.39elapsed 98%CPU (0avgtext+0avgdata 545844maxresident)k 3352inputs+13752outputs (7major+1044347minor)pagefaults 0swaps real 5m58.396s user 5m52.308s sys 0m2.036s + status=0 + set +x ================================================= data/session10/nastran_5_Flutter.py passed (as expected) ================================================= ================================================= aeroelastic_2_Iterative_SU2_Astros.py test; + time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.7.supp python aeroelastic_2_Iterative_SU2_Astros.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.7/CAPS/training/LINUX64/CAPS/training/training.log ==684475== Memcheck, a memory error detector ==684475== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==684475== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==684475== Command: python aeroelastic_2_Iterative_SU2_Astros.py ==684475== Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory Information: Dynamic Loader for scribeWake.so not found scribeWake.so: cannot open shared object file: No such file or directory ==> Running SU2 pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 03/14/23 @ 08:39PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.4.5 AFLR4 : Version Date 04/20/23 @ 05:37PM AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 04/21/23 @ 12:00AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 10 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 6 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 EGADS : 2 Yes 0 0 1 1 1 1 3 5 EGADS : 3 Yes 0 0 1 1 1 1 2 EGADS : 4 Yes 0 0 1 1 1 1 5 6 EGADS : 5 Yes 0 0 1 1 1 2 4 6 EGADS : 6 Yes 0 0 1 1 1 4 5 EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10 EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -3 5 1 -6 EGADS : 3 4 6 EGADS : 4 7 9 -8 -2 EGADS : 5 8 10 -7 -5 EGADS : 6 -9 -10 EGADS : 7 11 12 -13 -14 EGADS : 8 -15 18 17 -16 EGADS : 9 19 15 -20 -11 EGADS : 10 -21 13 22 -17 EGADS : 11 14 21 -18 -19 EGADS : 12 -12 20 16 -22 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 2 3 -4 EGADS : 2 Yes 1 -3 5 1 -6 EGADS : 3 Yes 1 4 6 EGADS : 4 Yes 1 7 9 -8 -2 EGADS : 5 Yes 1 8 10 -7 -5 EGADS : 6 Yes 1 -9 -10 EGADS : 7 Yes 1 11 12 -13 -14 EGADS : 8 Yes 1 -15 18 17 -16 EGADS : 9 Yes 1 19 15 -20 -11 EGADS : 10 Yes 1 -21 13 22 -17 EGADS : 11 Yes 1 14 21 -18 -19 EGADS : 12 Yes 1 -12 20 16 -22 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 2 EGADS : 2 0 Yes 1 3 1 1 4 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 5 EGADS : 6 0 Yes 4 2 1 2 3 EGADS : 7 0 Yes 1 5 1 4 5 EGADS : 8 0 Yes 3 6 1 4 5 EGADS : 9 0 Yes 5 6 1 4 6 EGADS : 10 0 Yes 6 5 1 5 6 EGADS : 11 1 Yes 8 7 NA 7 9 EGADS : 12 1 Yes 7 9 NA 7 12 EGADS : 13 1 Yes 10 9 NA 7 10 EGADS : 14 1 Yes 8 10 NA 7 11 EGADS : 15 1 Yes 12 11 NA 8 9 EGADS : 16 1 Yes 11 13 NA 8 12 EGADS : 17 1 Yes 14 13 NA 8 10 EGADS : 18 1 Yes 12 14 NA 8 11 EGADS : 19 1 Yes 8 12 NA 9 11 EGADS : 20 1 Yes 7 11 NA 9 12 EGADS : 21 1 Yes 10 14 NA 10 11 EGADS : 22 1 Yes 9 13 NA 10 12 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 1.61374306 0 0 EGADS : 2 Yes 2.37421202 0 0.355213563 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 1.40965066 0 0.270825378 EGADS : 5 Yes 2.37421202 3.87298335 0.355213563 EGADS : 6 Yes 1.40965066 3.87298335 0.270825378 EGADS : 7 Yes 0 0 77.6430368 EGADS : 8 Yes 0 0 0 EGADS : 9 Yes 0 77.4596689 77.6430368 EGADS : 10 Yes 0 77.4596689 0 EGADS : 11 Yes 78.6462641 0 77.6430368 EGADS : 12 Yes 78.6462641 0 0 EGADS : 13 Yes 78.6462641 77.4596689 77.6430368 EGADS : 14 Yes 78.6462641 77.4596689 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found EGADS : No Edge Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 154.919 AFLR4 : Min Bounding Box Length = 154.919 AFLR4 : Max Ref Bounding Box Length = 7.74597 AFLR4 : Min Ref Bounding Box Length = 0.433058 AFLR4 : Reference Length = 6.45497 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 21.0478 AFLR4 : Abs Min Surf Spacing = 0.0161374 AFLR4 : Min Surf Spacing = 0.0322749 AFLR4 : Max Surf Spacing = 0.645497 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : 10 CAD geometry 0 FARFIELD AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1658 3135 0 AFLR4 : Nodes, Trias,Quads= 971 1761 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1628 3077 0 AFLR4 : Nodes, Trias,Quads= 941 1703 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 48 65 0 AFLR4 : Nodes, Trias,Quads= 44 57 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1668 3155 0 AFLR4 : Nodes, Trias,Quads= 986 1791 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1625 3071 0 AFLR4 : Nodes, Trias,Quads= 930 1681 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 48 65 0 AFLR4 : Nodes, Trias,Quads= 44 57 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 3847 7686 938 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 3847 7686 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 3367 6423 0 AFLR4 : Nodes, Trias,Quads= 2401 4491 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 3394 6478 0 AFLR4 : Nodes, Trias,Quads= 2282 4254 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 145 226 0 AFLR4 : Nodes, Trias,Quads= 131 198 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 3366 6421 0 AFLR4 : Nodes, Trias,Quads= 2394 4477 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 3405 6500 0 AFLR4 : Nodes, Trias,Quads= 2289 4268 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 145 226 0 AFLR4 : Nodes, Trias,Quads= 131 198 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9265 18522 1526 OVERALL : CPU Time = 7.115 seconds Body 1 (of 2) Number of nodes = 8945 Number of elements = 17886 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 17886 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 320 Number of elements = 636 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9265 Total number of elements = 18522 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 03/14/23 @ 08:39PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.4.5 AFLR4 : Version Date 04/20/23 @ 05:37PM AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 04/21/23 @ 12:00AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9265 18522 1526 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.39 AFLR3 : Version Date 03/10/23 @ 04:32PM AFLR3 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR3 : Compile Date 03/14/23 @ 08:40PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 9265 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 FarField UG3 : 8 FarField UG3 : 9 FarField UG3 : 10 FarField UG3 : 11 FarField UG3 : 12 FarField AFLR3 : CPU Time = 0.513 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 9265 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1854 12666 AFLR3 IG : Nodes, Elements = 3708 26130 AFLR3 IG : Nodes, Elements = 5562 39589 AFLR3 IG : Nodes, Elements = 7416 54244 AFLR3 IG : Nodes, Elements = 9270 69463 AFLR3 IG : Nodes, Elements = 9272 69530 AFLR3 IG : Nodes, Elements = 9272 69335 AFLR3 IG : Nodes, Elements = 9265 42285 AFLR3 IG : Nodes, Elements = 9265 42353 AFLR3 IG : Nodes, Elements = 9265 30496 AFLR3 IG : Nodes, Elements = 9265 28301 AFLR3 : CPU Time = 5.284 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 9265 28301 AFLR3 GG : Nodes, Elements = 13542 41195 AFLR3 GG : Nodes, Elements = 13542 58908 AFLR3 GG : Nodes, Elements = 13542 54250 AFLR3 GG : Nodes, Elements = 17058 65245 AFLR3 GG : Nodes, Elements = 17058 78728 AFLR3 GG : Nodes, Elements = 17058 74303 AFLR3 GG : Nodes, Elements = 20605 85295 AFLR3 GG : Nodes, Elements = 20605 99195 AFLR3 GG : Nodes, Elements = 20605 94904 AFLR3 GG : Nodes, Elements = 24311 106150 AFLR3 GG : Nodes, Elements = 24311 121010 AFLR3 GG : Nodes, Elements = 24311 116688 AFLR3 GG : Nodes, Elements = 28109 128222 AFLR3 GG : Nodes, Elements = 28109 143116 AFLR3 GG : Nodes, Elements = 28109 139085 AFLR3 GG : Nodes, Elements = 31833 150343 AFLR3 GG : Nodes, Elements = 31833 164956 AFLR3 GG : Nodes, Elements = 31833 161115 AFLR3 GG : Nodes, Elements = 35425 171944 AFLR3 GG : Nodes, Elements = 35425 186053 AFLR3 GG : Nodes, Elements = 35425 182380 AFLR3 GG : Nodes, Elements = 38915 192902 AFLR3 GG : Nodes, Elements = 38915 206546 AFLR3 GG : Nodes, Elements = 38915 203031 AFLR3 GG : Nodes, Elements = 42279 213161 AFLR3 GG : Nodes, Elements = 42279 226492 AFLR3 GG : Nodes, Elements = 42279 223051 AFLR3 GG : Nodes, Elements = 45563 232931 AFLR3 GG : Nodes, Elements = 45563 245768 AFLR3 GG : Nodes, Elements = 45563 242514 AFLR3 GG : Nodes, Elements = 48695 251935 AFLR3 GG : Nodes, Elements = 48695 264207 AFLR3 GG : Nodes, Elements = 48695 261088 AFLR3 GG : Nodes, Elements = 51591 269788 AFLR3 GG : Nodes, Elements = 51591 281183 AFLR3 GG : Nodes, Elements = 51591 278253 AFLR3 GG : Nodes, Elements = 54386 286650 AFLR3 GG : Nodes, Elements = 54386 297696 AFLR3 GG : Nodes, Elements = 54386 294892 AFLR3 GG : Nodes, Elements = 57084 303004 AFLR3 GG : Nodes, Elements = 57084 313644 AFLR3 GG : Nodes, Elements = 57084 310937 AFLR3 GG : Nodes, Elements = 59614 318534 AFLR3 GG : Nodes, Elements = 59614 328459 AFLR3 GG : Nodes, Elements = 59614 326028 AFLR3 GG : Nodes, Elements = 61932 332987 AFLR3 GG : Nodes, Elements = 61932 342053 AFLR3 GG : Nodes, Elements = 61932 339758 AFLR3 GG : Nodes, Elements = 64173 346486 AFLR3 GG : Nodes, Elements = 64173 355203 AFLR3 GG : Nodes, Elements = 64173 353091 AFLR3 GG : Nodes, Elements = 66220 359236 AFLR3 GG : Nodes, Elements = 66220 367234 AFLR3 GG : Nodes, Elements = 66220 365224 AFLR3 GG : Nodes, Elements = 68183 371120 AFLR3 GG : Nodes, Elements = 68183 378771 AFLR3 GG : Nodes, Elements = 68183 376893 AFLR3 GG : Nodes, Elements = 70021 382413 AFLR3 GG : Nodes, Elements = 70021 389635 AFLR3 GG : Nodes, Elements = 70021 387894 AFLR3 GG : Nodes, Elements = 71738 393050 AFLR3 GG : Nodes, Elements = 71738 399670 AFLR3 GG : Nodes, Elements = 71738 398113 AFLR3 GG : Nodes, Elements = 73289 402770 AFLR3 GG : Nodes, Elements = 73289 408828 AFLR3 GG : Nodes, Elements = 73289 407358 AFLR3 GG : Nodes, Elements = 74785 411846 AFLR3 GG : Nodes, Elements = 74785 417552 AFLR3 GG : Nodes, Elements = 74785 416226 AFLR3 GG : Nodes, Elements = 76147 420314 AFLR3 GG : Nodes, Elements = 76147 425638 AFLR3 GG : Nodes, Elements = 76147 424379 AFLR3 GG : Nodes, Elements = 77386 428096 AFLR3 GG : Nodes, Elements = 77386 432940 AFLR3 GG : Nodes, Elements = 77386 431774 AFLR3 GG : Nodes, Elements = 78483 435067 AFLR3 GG : Nodes, Elements = 78483 439378 AFLR3 GG : Nodes, Elements = 78483 438266 AFLR3 GG : Nodes, Elements = 79434 441119 AFLR3 GG : Nodes, Elements = 79434 444842 AFLR3 GG : Nodes, Elements = 79434 443913 AFLR3 GG : Nodes, Elements = 80223 446281 AFLR3 GG : Nodes, Elements = 80223 449423 AFLR3 GG : Nodes, Elements = 80223 448600 AFLR3 GG : Nodes, Elements = 80840 450451 AFLR3 GG : Nodes, Elements = 80840 452964 AFLR3 GG : Nodes, Elements = 80840 452292 AFLR3 GG : Nodes, Elements = 81284 453624 AFLR3 GG : Nodes, Elements = 81284 455393 AFLR3 GG : Nodes, Elements = 81284 454894 AFLR3 GG : Nodes, Elements = 81599 455839 AFLR3 GG : Nodes, Elements = 81599 457118 AFLR3 GG : Nodes, Elements = 81599 456750 AFLR3 GG : Nodes, Elements = 81779 457290 AFLR3 GG : Nodes, Elements = 81779 458010 AFLR3 GG : Nodes, Elements = 81779 457813 AFLR3 GG : Nodes, Elements = 81888 458140 AFLR3 GG : Nodes, Elements = 81888 458622 AFLR3 GG : Nodes, Elements = 81888 458452 AFLR3 GG : Nodes, Elements = 81937 458599 AFLR3 GG : Nodes, Elements = 81937 458810 AFLR3 GG : Nodes, Elements = 81937 458739 AFLR3 GG : Nodes, Elements = 81953 458787 AFLR3 GG : Nodes, Elements = 81953 458858 AFLR3 GG : Nodes, Elements = 81953 458828 AFLR3 GG : Nodes, Elements = 81961 458852 AFLR3 GG : Nodes, Elements = 81961 458887 AFLR3 GG : Nodes, Elements = 81961 458871 AFLR3 GG : Nodes, Elements = 81966 458886 AFLR3 GG : Nodes, Elements = 81966 458898 AFLR3 GG : Nodes, Elements = 81966 458893 AFLR3 GG : Nodes, Elements = 81968 458899 AFLR3 GG : Nodes, Elements = 81968 458905 AFLR3 GG : Nodes, Elements = 81968 458903 AFLR3 : CPU Time = 1.611 minutes AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 81968 458903 AFLR3 QI : Nodes, Elements = 81513 456317 AFLR3 QI : Nodes, Elements = 81426 455827 AFLR3 QI : Nodes, Elements = 81418 455777 AFLR3 QI : Nodes, Elements = 81416 455768 AFLR3 QI : Nodes, Elements = 81416 457723 AFLR3 QI : Nodes, Elements = 81416 455611 AFLR3 QI : Nodes, Elements = 81416 454711 AFLR3 QI : Nodes, Elements = 81416 454979 AFLR3 QI : Nodes, Elements = 81416 454537 AFLR3 QI : Nodes, Elements = 81416 454422 AFLR3 : CPU Time = 26.835 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 454422 UG3 : Min, Max Ang = 12.41 159.2 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 3.72e+06 UG3 : No. Tet Elems = 454422 UG3 : Min Vol = 1.01e-06 UG3 : Average Vol = 8.18 UG3 : Total-Tet-Vol = 3.72e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 454422 UG3 : Min, Max Q = 0.205 1 UG3 : Average Q = 0.896 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 2.251 minutes UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 454422 UG3 : Min, Max Ang = 12.41 159.2 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 0 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 3.72e+06 UG3 : No. Tet Elems = 454422 UG3 : Min Vol = 1.01e-06 UG3 : Average Vol = 8.18 UG3 : Total-Tet-Vol = 3.72e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 454422 UG3 : Min, Max Q = 0.361 1 UG3 : Average Q = 0.863 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 13 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 14 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 15 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 7 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 8 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 7 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 8 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12 Volume mesh: Number of nodes = 81416 Number of elements = 472944 Number of triangles = 18522 Number of quadrilatarals = 0 Number of tetrahedrals = 454422 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticIterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... /home/jenkins/util/SU2/SU2-v7.5.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='aeroelasticIterative.cfg' mode='r' encoding='UTF-8'> konfig = read_config(filename) ResourceWarning: Enable tracemalloc to get the object allocation traceback /home/jenkins/util/SU2/SU2-v7.5.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'> for raw_line in open(temp_filename): ResourceWarning: Enable tracemalloc to get the object allocation traceback ==687063== Warning: invalid file descriptor 1048564 in syscall close() ==687063== Warning: invalid file descriptor 1048565 in syscall close() ==687063== Warning: invalid file descriptor 1048566 in syscall close() ==687063== Warning: invalid file descriptor 1048567 in syscall close() ==687063== Use --log-fd=<number> to select an alternative log fd. ==687063== Warning: invalid file descriptor 1048568 in syscall close() ==687063== Warning: invalid file descriptor 1048569 in syscall close() ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 10 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 7.74597 m. Reference origin for moment evaluation is (0.322749, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 81416 grid points. 454422 volume elements. 2 surface markers. 17886 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 454422 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 3.71806e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 431.689. Mean K: 20.6913. Standard deviation K: 49.4454. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 51.1523| 86.7063| | CV Face Area Aspect Ratio| 1.04012| 115.282| | CV Sub-Volume Ratio| 1| 701.712| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 81416| 1/1.00| 10| | 1| 13392| 1/6.08| 8.2187| | 2| 2069| 1/6.47| 6.61504| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.52985 m^2, y-plane = 0.868532 m^2, z-plane = 9.83638 m^2. Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m. Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.9914e+00| -1.762880| 0.455100| 0.055818| 3.706226| -0.552238| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.9246e+00| -1.567620| 0.800265| 0.530357| 3.903824| -0.295493| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.8932e+00| -1.601362| 0.945584| 0.763508| 3.871421| 1.801614| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.9128e+00| -1.681553| 0.931856| 0.796718| 3.784455| -8.276542| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.0487e+00| -1.622632| 0.831000| 0.682309| 3.844421| -5.286333| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.62263| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ /home/jenkins/util/SU2/SU2-v7.5.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4> run_command( the_Command ) ResourceWarning: Enable tracemalloc to get the object allocation traceback ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 265 Number of elements = 346 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 346 ---------------------------- Total number of nodes = 265 Total number of elements = 346 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 265 Number of elements = 346 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 346 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses CAPS Info: Reparameterization Bound -> upperWing -- nu, nv = 129 129 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.247769e+09, tgt = 6.247769e+09, diff = 6.274147e-01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.100462e+09, tgt = 6.100462e+09, diff = 2.016616e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.121567e+07, tgt = 6.121567e+07, diff = 1.005828e-06 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.124703e+07, tgt = 6.124703e+07, diff = 1.490116e-08 Extracting external pressure loads from data transfer.... TransferName = upperWing Number of Elements = 96 (total = 96) TransferName = lowerWing Number of Elements = 96 (total = 192) TransferName = leftTip Number of Elements = 10 (total = 202) TransferName = riteTip Number of Elements = 10 (total = 212) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards Running mASTROS...... ==> Running ASTROS post-analysis... ==> Running SU2 pre-analysis... Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticIterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2...... /home/jenkins/util/SU2/SU2-v7.5.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_DEF.cfg_tmp' mode='r' encoding='UTF-8'> for raw_line in open(temp_filename): ResourceWarning: Enable tracemalloc to get the object allocation traceback ==702762== Warning: invalid file descriptor 1048564 in syscall close() ==702762== Warning: invalid file descriptor 1048565 in syscall close() ==702762== Warning: invalid file descriptor 1048566 in syscall close() ==702762== Warning: invalid file descriptor 1048567 in syscall close() ==702762== Use --log-fd=<number> to select an alternative log fd. ==702762== Warning: invalid file descriptor 1048568 in syscall close() ==702762== Warning: invalid file descriptor 1048569 in syscall close() ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_0.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: aeroelasticIterative.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 81416 grid points. 454422 volume elements. 2 surface markers. 17886 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 454422 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 3.71806e+06. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). ----------------------- Write deformed grid files ----------------------- |SU2 mesh |aeroelasticIterative.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Solver Postprocessing ------------------------- Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. Completed in 27.095663 seconds on 1 core. ------------------------- Exit Success (SU2_DEF) ------------------------ /home/jenkins/util/SU2/SU2-v7.5.1/bin/SU2/run/interface.py:133: ResourceWarning: unclosed file <_io.BufferedReader name=4> run_command( the_Command ) ResourceWarning: Enable tracemalloc to get the object allocation traceback ==707138== Warning: invalid file descriptor 1048564 in syscall close() ==707138== Warning: invalid file descriptor 1048565 in syscall close() ==707138== Warning: invalid file descriptor 1048566 in syscall close() ==707138== Warning: invalid file descriptor 1048567 in syscall close() ==707138== Use --log-fd=<number> to select an alternative log fd. ==707138== Warning: invalid file descriptor 1048568 in syscall close() ==707138== Warning: invalid file descriptor 1048569 in syscall close() ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 10 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 7.74597 m. Reference origin for moment evaluation is (0.322749, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 81416 grid points. 454422 volume elements. 2 surface markers. 17886 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 454422 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 3.71806e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 431.689. Mean K: 20.6913. Standard deviation K: 49.4454. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 51.1523| 86.7063| | CV Face Area Aspect Ratio| 1.04012| 115.282| | CV Sub-Volume Ratio| 1| 701.712| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 81416| 1/1.00| 10| | 1| 13392| 1/6.08| 8.2187| | 2| 2069| 1/6.47| 6.61504| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.52985 m^2, y-plane = 0.868532 m^2, z-plane = 9.83638 m^2. Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m. Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.4941e+00| -1.762880| 0.455100| 0.055818| 3.706226| -0.552238| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.4171e+00| -1.567620| 0.800265| 0.530357| 3.903824| -0.295493| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.3792e+00| -1.601362| 0.945584| 0.763508| 3.871421| 1.801614| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.2833e+00| -1.681553| 0.931856| 0.796718| 3.784455| -8.276542| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.1986e+00| -1.622632| 0.831000| 0.682309| 3.844421| -5.286333| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.62263| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.247769e+09, tgt = 6.247769e+09, diff = 6.274147e-01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.100462e+09, tgt = 6.100462e+09, diff = 2.016616e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.121567e+07, tgt = 6.121567e+07, diff = 1.005828e-06 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.124703e+07, tgt = 6.124703e+07, diff = 1.490116e-08 Extracting external pressure loads from data transfer.... TransferName = upperWing Number of Elements = 96 (total = 96) TransferName = lowerWing Number of Elements = 96 (total = 192) TransferName = leftTip Number of Elements = 10 (total = 202) TransferName = riteTip Number of Elements = 10 (total = 212) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards Running mASTROS...... ==> Running ASTROS post-analysis... ==684475== ==684475== HEAP SUMMARY: ==684475== in use at exit: 4,333,904 bytes in 24,930 blocks ==684475== total heap usage: 15,795,796 allocs, 15,770,866 frees, 112,921,113,031 bytes allocated ==684475== ==684475== LEAK SUMMARY: ==684475== definitely lost: 0 bytes in 0 blocks ==684475== indirectly lost: 0 bytes in 0 blocks ==684475== possibly lost: 0 bytes in 0 blocks ==684475== still reachable: 0 bytes in 0 blocks ==684475== suppressed: 4,333,904 bytes in 24,930 blocks ==684475== ==684475== For lists of detected and suppressed errors, rerun with: -s ==684475== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1907 from 1907) 1385.02user 22.81system 23:23.16elapsed 100%CPU (0avgtext+0avgdata 4360256maxresident)k 9352inputs+327664outputs (44major+10314448minor)pagefaults 0swaps real 23m23.167s user 23m5.024s sys 0m22.847s + status=0 + set +x ================================================= data/session11/aeroelastic_2_Iterative_SU2_Astros.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: session08 fun3d session11 fun3d+astros ================================================= ================================================= Summary of examples NOT finished as expected data/session07/pointwise_01_Defaults.py data/session07/pointwise_02_InviscidWing.py data/session07/pointwise_03_TurnAngle.py data/session07/pointwise_04_TurnAngleHard.py data/session07/pointwise_05_DomainDecay.py data/session07/pointwise_06_ConnectorProximity.py data/session07/pointwise_07_InviscidTransport.py data/session07/pointwise_08_ViscousWing.py solutions/session07/pointwise_DomainProximity.py See training.log for more details. ================================================= Build step 'Conditional step (single)' marked build as failure [GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE' [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: FAILURE