The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 2,522 KB.. Full LogNumber of line elements = 0 Number of triangle elements = 17115 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 8266 Total number of elements = 17115 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/7.4/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 = 1566 Number of elements = 3043 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3043 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1566 Total number of elements = 3043 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 ==1765785== ==1765785== HEAP SUMMARY: ==1765785== in use at exit: 4,093,990 bytes in 24,484 blocks ==1765785== total heap usage: 34,000,739 allocs, 33,976,255 frees, 10,570,131,057 bytes allocated ==1765785== ==1765785== LEAK SUMMARY: ==1765785== definitely lost: 0 bytes in 0 blocks ==1765785== indirectly lost: 0 bytes in 0 blocks ==1765785== possibly lost: 0 bytes in 0 blocks ==1765785== still reachable: 0 bytes in 0 blocks ==1765785== suppressed: 4,093,990 bytes in 24,484 blocks ==1765785== ==1765785== For lists of detected and suppressed errors, rerun with: -s ==1765785== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1874 from 1874) 542.19user 2.25system 9:04.19elapsed 100%CPU (0avgtext+0avgdata 593492maxresident)k 8inputs+104104outputs (0major+1460905minor)pagefaults 0swaps real 9m4.193s user 9m2.200s sys 0m2.256s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python tess_7_MeshSizing.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1766206== Memcheck, a memory error detector ==1766206== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1766206== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1766206== Command: python tess_7_MeshSizing.py ==1766206== ==> 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/7.4/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 = 8266 Number of elements = 17115 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 17115 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 8266 Total number of elements = 17115 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 = 3860 Number of elements = 8288 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 8288 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3860 Total number of elements = 8288 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 ==1766206== ==1766206== HEAP SUMMARY: ==1766206== in use at exit: 4,094,362 bytes in 24,489 blocks ==1766206== total heap usage: 21,536,941 allocs, 21,512,452 frees, 6,718,047,964 bytes allocated ==1766206== ==1766206== LEAK SUMMARY: ==1766206== definitely lost: 0 bytes in 0 blocks ==1766206== indirectly lost: 0 bytes in 0 blocks ==1766206== possibly lost: 0 bytes in 0 blocks ==1766206== still reachable: 0 bytes in 0 blocks ==1766206== suppressed: 4,094,362 bytes in 24,489 blocks ==1766206== ==1766206== For lists of detected and suppressed errors, rerun with: -s ==1766206== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1876 from 1876) 378.77user 1.73system 6:20.25elapsed 100%CPU (0avgtext+0avgdata 554316maxresident)k 8inputs+40872outputs (0major+1069915minor)pagefaults 0swaps real 6m20.253s user 6m18.780s sys 0m1.736s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python tess_8_MeshSizing.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1766576== Memcheck, a memory error detector ==1766576== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1766576== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1766576== Command: python tess_8_MeshSizing.py ==1766576== ==> 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/7.4/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 = 1566 Number of elements = 3043 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3043 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1566 Total number of elements = 3043 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 = 6582 Number of elements = 13186 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 13186 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 6582 Total number of elements = 13186 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 = 22194 Number of elements = 22195 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 22195 ---------------------------- Total number of nodes = 22194 Total number of elements = 22195 ==1766576== ==1766576== HEAP SUMMARY: ==1766576== in use at exit: 4,094,362 bytes in 24,489 blocks ==1766576== total heap usage: 23,570,235 allocs, 23,545,746 frees, 6,751,739,090 bytes allocated ==1766576== ==1766576== LEAK SUMMARY: ==1766576== definitely lost: 0 bytes in 0 blocks ==1766576== indirectly lost: 0 bytes in 0 blocks ==1766576== possibly lost: 0 bytes in 0 blocks ==1766576== still reachable: 0 bytes in 0 blocks ==1766576== suppressed: 4,094,362 bytes in 24,489 blocks ==1766576== ==1766576== For lists of detected and suppressed errors, rerun with: -s ==1766576== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1876 from 1876) 392.69user 1.84system 6:34.28elapsed 100%CPU (0avgtext+0avgdata 595988maxresident)k 8inputs+43736outputs (0major+1224558minor)pagefaults 0swaps real 6m34.291s user 6m32.700s sys 0m1.846s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python tess_MinQuad.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1766869== Memcheck, a memory error detector ==1766869== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1766869== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1766869== Command: python tess_MinQuad.py ==1766869== ==> 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/7.4/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 ==1766869== ==1766869== HEAP SUMMARY: ==1766869== in use at exit: 4,093,734 bytes in 24,484 blocks ==1766869== total heap usage: 16,286,018 allocs, 16,261,534 frees, 5,128,007,873 bytes allocated ==1766869== ==1766869== LEAK SUMMARY: ==1766869== definitely lost: 0 bytes in 0 blocks ==1766869== indirectly lost: 0 bytes in 0 blocks ==1766869== possibly lost: 0 bytes in 0 blocks ==1766869== still reachable: 0 bytes in 0 blocks ==1766869== suppressed: 4,093,734 bytes in 24,484 blocks ==1766869== ==1766869== For lists of detected and suppressed errors, rerun with: -s ==1766869== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1875 from 1875) 300.79user 1.39system 5:01.98elapsed 100%CPU (0avgtext+0avgdata 547652maxresident)k 8inputs+12624outputs (0major+921899minor)pagefaults 0swaps real 5m1.983s user 5m0.803s sys 0m1.396s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python tess_2k.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1767119== Memcheck, a memory error detector ==1767119== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1767119== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1767119== Command: python tess_2k.py ==1767119== ==> 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/7.4/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 ==1767119== ==1767119== HEAP SUMMARY: ==1767119== in use at exit: 4,094,213 bytes in 24,487 blocks ==1767119== total heap usage: 18,073,817 allocs, 18,049,330 frees, 5,665,930,104 bytes allocated ==1767119== ==1767119== LEAK SUMMARY: ==1767119== definitely lost: 0 bytes in 0 blocks ==1767119== indirectly lost: 0 bytes in 0 blocks ==1767119== possibly lost: 0 bytes in 0 blocks ==1767119== still reachable: 0 bytes in 0 blocks ==1767119== suppressed: 4,094,213 bytes in 24,487 blocks ==1767119== ==1767119== For lists of detected and suppressed errors, rerun with: -s ==1767119== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1875 from 1875) 312.41user 1.51system 5:13.72elapsed 100%CPU (0avgtext+0avgdata 559520maxresident)k 8inputs+11352outputs (0major+843871minor)pagefaults 0swaps real 5m13.731s user 5m12.422s sys 0m1.513s + status=0 + set +x ================================================= solutions/session09/tess_2k.py passed (as expected) ================================================= ================================================= astros_1_ModalClamped.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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python astros_1_ModalClamped.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1767374== Memcheck, a memory error detector ==1767374== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1767374== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1767374== Command: python astros_1_ModalClamped.py ==1767374== ==> 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/7.4/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 = 9 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 --> 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 ==1767374== ==1767374== HEAP SUMMARY: ==1767374== in use at exit: 4,096,357 bytes in 24,497 blocks ==1767374== total heap usage: 17,780,575 allocs, 17,756,078 frees, 5,591,152,496 bytes allocated ==1767374== ==1767374== LEAK SUMMARY: ==1767374== definitely lost: 0 bytes in 0 blocks ==1767374== indirectly lost: 0 bytes in 0 blocks ==1767374== possibly lost: 0 bytes in 0 blocks ==1767374== still reachable: 0 bytes in 0 blocks ==1767374== suppressed: 4,096,357 bytes in 24,497 blocks ==1767374== ==1767374== For lists of detected and suppressed errors, rerun with: -s ==1767374== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1880 from 1880) 310.24user 1.56system 5:11.65elapsed 100%CPU (0avgtext+0avgdata 556080maxresident)k 16inputs+38544outputs (0major+809287minor)pagefaults 0swaps real 5m11.662s user 5m10.243s sys 0m1.575s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python astros_2_ModalSupport.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1767605== Memcheck, a memory error detector ==1767605== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1767605== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1767605== Command: python astros_2_ModalSupport.py ==1767605== ==> 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/7.4/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 ==1767605== ==1767605== HEAP SUMMARY: ==1767605== in use at exit: 4,096,357 bytes in 24,497 blocks ==1767605== total heap usage: 17,781,735 allocs, 17,757,238 frees, 5,611,834,974 bytes allocated ==1767605== ==1767605== LEAK SUMMARY: ==1767605== definitely lost: 0 bytes in 0 blocks ==1767605== indirectly lost: 0 bytes in 0 blocks ==1767605== possibly lost: 0 bytes in 0 blocks ==1767605== still reachable: 0 bytes in 0 blocks ==1767605== suppressed: 4,096,357 bytes in 24,497 blocks ==1767605== ==1767605== For lists of detected and suppressed errors, rerun with: -s ==1767605== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1878 from 1878) 310.52user 1.46system 5:11.81elapsed 100%CPU (0avgtext+0avgdata 558684maxresident)k 16inputs+40360outputs (0major+807288minor)pagefaults 0swaps real 5m11.814s user 5m10.535s sys 0m1.463s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python astros_3_StaticClamped.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1767871== Memcheck, a memory error detector ==1767871== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1767871== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1767871== Command: python astros_3_StaticClamped.py ==1767871== ==> 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/7.4/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 43461.879146949635 --> T1max 738.595 --> T2max 3686.25 --> T3max 43363.8 ==1767871== ==1767871== HEAP SUMMARY: ==1767871== in use at exit: 4,096,357 bytes in 24,497 blocks ==1767871== total heap usage: 17,781,898 allocs, 17,757,401 frees, 5,591,309,034 bytes allocated ==1767871== ==1767871== LEAK SUMMARY: ==1767871== definitely lost: 0 bytes in 0 blocks ==1767871== indirectly lost: 0 bytes in 0 blocks ==1767871== possibly lost: 0 bytes in 0 blocks ==1767871== still reachable: 0 bytes in 0 blocks ==1767871== suppressed: 4,096,357 bytes in 24,497 blocks ==1767871== ==1767871== For lists of detected and suppressed errors, rerun with: -s ==1767871== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1877 from 1877) 308.71user 1.58system 5:10.14elapsed 100%CPU (0avgtext+0avgdata 557856maxresident)k 16inputs+34592outputs (0major+814668minor)pagefaults 0swaps real 5m10.143s user 5m8.717s sys 0m1.586s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python astros_4_Composite.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1768134== Memcheck, a memory error detector ==1768134== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1768134== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1768134== Command: python astros_4_Composite.py ==1768134== ==> 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/7.4/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 ==1768134== ==1768134== HEAP SUMMARY: ==1768134== in use at exit: 4,096,434 bytes in 24,498 blocks ==1768134== total heap usage: 17,782,709 allocs, 17,758,211 frees, 5,591,382,603 bytes allocated ==1768134== ==1768134== LEAK SUMMARY: ==1768134== definitely lost: 0 bytes in 0 blocks ==1768134== indirectly lost: 0 bytes in 0 blocks ==1768134== possibly lost: 0 bytes in 0 blocks ==1768134== still reachable: 0 bytes in 0 blocks ==1768134== suppressed: 4,096,434 bytes in 24,498 blocks ==1768134== ==1768134== For lists of detected and suppressed errors, rerun with: -s ==1768134== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1877 from 1877) 309.67user 1.50system 5:11.00elapsed 100%CPU (0avgtext+0avgdata 558620maxresident)k 16inputs+34576outputs (0major+876169minor)pagefaults 0swaps real 5m11.006s user 5m9.682s sys 0m1.503s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python nastran_5_Flutter.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1768424== Memcheck, a memory error detector ==1768424== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1768424== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1768424== Command: python nastran_5_Flutter.py ==1768424== ==> 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 ==1768424== ==1768424== HEAP SUMMARY: ==1768424== in use at exit: 4,095,992 bytes in 24,493 blocks ==1768424== total heap usage: 14,891,465 allocs, 14,866,972 frees, 4,962,462,141 bytes allocated ==1768424== ==1768424== LEAK SUMMARY: ==1768424== definitely lost: 0 bytes in 0 blocks ==1768424== indirectly lost: 0 bytes in 0 blocks ==1768424== possibly lost: 0 bytes in 0 blocks ==1768424== still reachable: 0 bytes in 0 blocks ==1768424== suppressed: 4,095,992 bytes in 24,493 blocks ==1768424== ==1768424== For lists of detected and suppressed errors, rerun with: -s ==1768424== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1876 from 1876) 302.40user 1.40system 5:03.60elapsed 100%CPU (0avgtext+0avgdata 558276maxresident)k 16inputs+13744outputs (0major+829932minor)pagefaults 0swaps real 5m3.606s user 5m2.414s sys 0m1.408s + 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/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.4.supp python aeroelastic_2_Iterative_SU2_Astros.py + tee -a /jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64/CAPS/training/training.log ==1780741== Memcheck, a memory error detector ==1780741== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==1780741== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==1780741== Command: python aeroelastic_2_Iterative_SU2_Astros.py ==1780741== 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 11.3.17 AFLR4 : Version Date 03/03/23 @ 03:12PM AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 03/14/23 @ 08:40PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 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 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= 6118 11925 0 AFLR4 : Nodes, Trias,Quads= 2408 4505 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 5960 11610 0 AFLR4 : Nodes, Trias,Quads= 2296 4282 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 147 230 0 AFLR4 : Nodes, Trias,Quads= 131 198 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 6173 12035 0 AFLR4 : Nodes, Trias,Quads= 2395 4479 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 6053 11796 0 AFLR4 : Nodes, Trias,Quads= 2292 4274 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 147 230 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= 9290 18572 1526 OVERALL : CPU Time = 6.866 seconds Body 1 (of 2) Number of nodes = 8970 Number of elements = 17936 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 17936 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 = 9290 Total number of elements = 18572 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 11.3.17 AFLR4 : Version Date 03/03/23 @ 03:12PM AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 03/14/23 @ 08:40PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 EGADS : --------------------------------------- DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9290 18572 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 = 9290 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 = 0.452 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 9290 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1860 12646 AFLR3 IG : Nodes, Elements = 3720 25971 AFLR3 IG : Nodes, Elements = 5580 39697 AFLR3 IG : Nodes, Elements = 7440 54213 AFLR3 IG : Nodes, Elements = 9297 69672 AFLR3 IG : Nodes, Elements = 9297 69492 AFLR3 IG : Nodes, Elements = 9290 42442 AFLR3 IG : Nodes, Elements = 9290 42501 AFLR3 IG : Nodes, Elements = 9290 30785 AFLR3 IG : Nodes, Elements = 9290 28628 AFLR3 : CPU Time = 4.509 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 9290 28628 AFLR3 GG : Nodes, Elements = 13561 41513 AFLR3 GG : Nodes, Elements = 13561 58358 AFLR3 GG : Nodes, Elements = 13561 53657 AFLR3 GG : Nodes, Elements = 17117 64735 AFLR3 GG : Nodes, Elements = 17117 78808 AFLR3 GG : Nodes, Elements = 17117 74279 AFLR3 GG : Nodes, Elements = 20675 85292 AFLR3 GG : Nodes, Elements = 20675 99081 AFLR3 GG : Nodes, Elements = 20675 94981 AFLR3 GG : Nodes, Elements = 24337 106153 AFLR3 GG : Nodes, Elements = 24337 120869 AFLR3 GG : Nodes, Elements = 24337 116773 AFLR3 GG : Nodes, Elements = 28106 128236 AFLR3 GG : Nodes, Elements = 28106 142965 AFLR3 GG : Nodes, Elements = 28106 139010 AFLR3 GG : Nodes, Elements = 31766 150079 AFLR3 GG : Nodes, Elements = 31766 164489 AFLR3 GG : Nodes, Elements = 31766 160588 AFLR3 GG : Nodes, Elements = 35380 171500 AFLR3 GG : Nodes, Elements = 35380 185811 AFLR3 GG : Nodes, Elements = 35380 182124 AFLR3 GG : Nodes, Elements = 38823 192508 AFLR3 GG : Nodes, Elements = 38823 206006 AFLR3 GG : Nodes, Elements = 38823 202470 AFLR3 GG : Nodes, Elements = 42134 212447 AFLR3 GG : Nodes, Elements = 42134 225390 AFLR3 GG : Nodes, Elements = 42134 222178 AFLR3 GG : Nodes, Elements = 45345 231848 AFLR3 GG : Nodes, Elements = 45345 244494 AFLR3 GG : Nodes, Elements = 45345 241207 AFLR3 GG : Nodes, Elements = 48398 250392 AFLR3 GG : Nodes, Elements = 48398 262281 AFLR3 GG : Nodes, Elements = 48398 259327 AFLR3 GG : Nodes, Elements = 51273 267969 AFLR3 GG : Nodes, Elements = 51273 279340 AFLR3 GG : Nodes, Elements = 51273 276462 AFLR3 GG : Nodes, Elements = 54042 284789 AFLR3 GG : Nodes, Elements = 54042 295506 AFLR3 GG : Nodes, Elements = 54042 292883 AFLR3 GG : Nodes, Elements = 56636 300683 AFLR3 GG : Nodes, Elements = 56636 310952 AFLR3 GG : Nodes, Elements = 56636 308342 AFLR3 GG : Nodes, Elements = 59123 315811 AFLR3 GG : Nodes, Elements = 59123 325722 AFLR3 GG : Nodes, Elements = 59123 323181 AFLR3 GG : Nodes, Elements = 61483 330272 AFLR3 GG : Nodes, Elements = 61483 339606 AFLR3 GG : Nodes, Elements = 61483 337245 AFLR3 GG : Nodes, Elements = 63678 343841 AFLR3 GG : Nodes, Elements = 63678 352418 AFLR3 GG : Nodes, Elements = 63678 350277 AFLR3 GG : Nodes, Elements = 65758 356528 AFLR3 GG : Nodes, Elements = 65758 364558 AFLR3 GG : Nodes, Elements = 65758 362578 AFLR3 GG : Nodes, Elements = 67790 368681 AFLR3 GG : Nodes, Elements = 67790 376603 AFLR3 GG : Nodes, Elements = 67790 374718 AFLR3 GG : Nodes, Elements = 69606 380169 AFLR3 GG : Nodes, Elements = 69606 387298 AFLR3 GG : Nodes, Elements = 69606 385523 AFLR3 GG : Nodes, Elements = 71286 390568 AFLR3 GG : Nodes, Elements = 71286 397091 AFLR3 GG : Nodes, Elements = 71286 395493 AFLR3 GG : Nodes, Elements = 72871 400253 AFLR3 GG : Nodes, Elements = 72871 406495 AFLR3 GG : Nodes, Elements = 72871 404928 AFLR3 GG : Nodes, Elements = 74289 409183 AFLR3 GG : Nodes, Elements = 74289 414668 AFLR3 GG : Nodes, Elements = 74289 413342 AFLR3 GG : Nodes, Elements = 75656 417447 AFLR3 GG : Nodes, Elements = 75656 422806 AFLR3 GG : Nodes, Elements = 75656 421489 AFLR3 GG : Nodes, Elements = 76889 425188 AFLR3 GG : Nodes, Elements = 76889 430052 AFLR3 GG : Nodes, Elements = 76889 428849 AFLR3 GG : Nodes, Elements = 78048 432330 AFLR3 GG : Nodes, Elements = 78048 436850 AFLR3 GG : Nodes, Elements = 78048 435708 AFLR3 GG : Nodes, Elements = 79141 438988 AFLR3 GG : Nodes, Elements = 79141 443321 AFLR3 GG : Nodes, Elements = 79141 442273 AFLR3 GG : Nodes, Elements = 80177 445384 AFLR3 GG : Nodes, Elements = 80177 449363 AFLR3 GG : Nodes, Elements = 80177 448421 AFLR3 GG : Nodes, Elements = 81132 451286 AFLR3 GG : Nodes, Elements = 81132 455027 AFLR3 GG : Nodes, Elements = 81132 454114 AFLR3 GG : Nodes, Elements = 81965 456616 AFLR3 GG : Nodes, Elements = 81965 459966 AFLR3 GG : Nodes, Elements = 81965 459099 AFLR3 GG : Nodes, Elements = 82658 461179 AFLR3 GG : Nodes, Elements = 82658 463902 AFLR3 GG : Nodes, Elements = 82658 463198 AFLR3 GG : Nodes, Elements = 83226 464902 AFLR3 GG : Nodes, Elements = 83226 467218 AFLR3 GG : Nodes, Elements = 83226 466581 AFLR3 GG : Nodes, Elements = 83659 467880 AFLR3 GG : Nodes, Elements = 83659 469692 AFLR3 GG : Nodes, Elements = 83659 469158 AFLR3 GG : Nodes, Elements = 83947 470023 AFLR3 GG : Nodes, Elements = 83947 471204 AFLR3 GG : Nodes, Elements = 83947 470847 AFLR3 GG : Nodes, Elements = 84133 471405 AFLR3 GG : Nodes, Elements = 84133 472156 AFLR3 GG : Nodes, Elements = 84133 471928 AFLR3 GG : Nodes, Elements = 84231 472222 AFLR3 GG : Nodes, Elements = 84231 472634 AFLR3 GG : Nodes, Elements = 84231 472491 AFLR3 GG : Nodes, Elements = 84273 472617 AFLR3 GG : Nodes, Elements = 84273 472798 AFLR3 GG : Nodes, Elements = 84273 472740 AFLR3 GG : Nodes, Elements = 84281 472764 AFLR3 GG : Nodes, Elements = 84281 472792 AFLR3 GG : Nodes, Elements = 84281 472781 AFLR3 GG : Nodes, Elements = 84287 472799 AFLR3 GG : Nodes, Elements = 84287 472813 AFLR3 GG : Nodes, Elements = 84287 472807 AFLR3 : CPU Time = 1.366 minutes AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 84287 472807 AFLR3 QI : Nodes, Elements = 83845 470306 AFLR3 QI : Nodes, Elements = 83783 469957 AFLR3 QI : Nodes, Elements = 83774 469906 AFLR3 QI : Nodes, Elements = 83774 471765 AFLR3 QI : Nodes, Elements = 83774 469695 AFLR3 QI : Nodes, Elements = 83774 468779 AFLR3 QI : Nodes, Elements = 83774 469030 AFLR3 QI : Nodes, Elements = 83774 468600 AFLR3 QI : Nodes, Elements = 83774 468491 AFLR3 QI : Nodes, Elements = 83774 468696 AFLR3 QI : Nodes, Elements = 83774 468475 AFLR3 QI : Nodes, Elements = 83774 468435 AFLR3 QI : Nodes, Elements = 83774 468615 AFLR3 QI : Nodes, Elements = 83774 468429 AFLR3 QI : Nodes, Elements = 83774 468397 AFLR3 QI : Nodes, Elements = 83774 468606 AFLR3 QI : Nodes, Elements = 83774 468421 AFLR3 QI : Nodes, Elements = 83774 468402 AFLR3 QI : Nodes, Elements = 83775 468406 AFLR3 QI : Nodes, Elements = 83775 468587 AFLR3 QI : Nodes, Elements = 83775 468408 AFLR3 QI : Nodes, Elements = 83775 468401 AFLR3 QI : Nodes, Elements = 83775 468610 AFLR3 QI : Nodes, Elements = 83775 468402 AFLR3 QI : Nodes, Elements = 83775 468381 AFLR3 : CPU Time = 40.589 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 468381 UG3 : Min, Max Ang = 13.82 158.3 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 = 468381 UG3 : Min Vol = 8.95e-07 UG3 : Average Vol = 7.94 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 = 468381 UG3 : Min, Max Q = 0.26 1 UG3 : Average Q = 0.902 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 2.212 minutes UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 468381 UG3 : Min, Max Ang = 13.82 158.3 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 = 468381 UG3 : Min Vol = 8.95e-07 UG3 : Average Vol = 7.94 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 = 468381 UG3 : Min, Max Q = 0.383 1 UG3 : Average Q = 0.874 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 7.4.1 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 = 83775 Number of elements = 486953 Number of triangles = 18572 Number of quadrilatarals = 0 Number of tetrahedrals = 468381 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 (7.4.0) " Running SU2...... /home/jenkins/util/SU2/SU2-v7.4.0/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-v7.4.0/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 ==1780920== Warning: invalid file descriptor 1048564 in syscall close() ==1780920== Warning: invalid file descriptor 1048565 in syscall close() ==1780920== Warning: invalid file descriptor 1048566 in syscall close() ==1780920== Warning: invalid file descriptor 1048567 in syscall close() ==1780920== Use --log-fd=<number> to select an alternative log fd. ==1780920== Warning: invalid file descriptor 1048568 in syscall close() ==1780920== Warning: invalid file descriptor 1048569 in syscall close() ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.4.0 "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 2012-2022, 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. 83775 grid points. 468381 volume elements. 2 surface markers. 17936 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 468381 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: 20.6394. Standard deviation K: 49.3925. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 47.2388| 86.636| | CV Face Area Aspect Ratio| 1.07945| 107.626| | CV Sub-Volume Ratio| 1| 835.999| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 83775| 1/1.00| 10| | 1| 13821| 1/6.06| 8.22684| | 2| 2125| 1/6.5| 6.61095| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.53011 m^2, y-plane = 0.868549 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 +----------------------------------------------------------------------------------------------------------------------------------------------+ | 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| 3.1589e+00| -1.769868| 0.448506| 0.049654| 3.699238| -0.549589| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.0884e+00| -1.514606| 0.839346| 0.462880| 3.962010| -0.289362| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.0612e+00| -1.526763| 0.926179| 0.740347| 3.939565| 1.925842| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.0414e+00| -1.606192| 0.945796| 0.806951| 3.854348| -8.538088| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.0249e+00| -1.480946| 0.895276| 0.699471| 3.988747| -5.572881| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.48095| < -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-v7.4.0/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 = 8970 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.249086e+09, tgt = 6.249086e+09, diff = 2.904410e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.101315e+09, tgt = 6.101315e+09, diff = 1.479870e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.122063e+07, tgt = 6.122063e+07, diff = 7.450581e-09 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.122314e+07, tgt = 6.122314e+07, diff = 0.000000e+00 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 (7.4.0) " Running SU2...... /home/jenkins/util/SU2/SU2-v7.4.0/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 ==1809378== Warning: invalid file descriptor 1048564 in syscall close() ==1809378== Warning: invalid file descriptor 1048565 in syscall close() ==1809378== Warning: invalid file descriptor 1048566 in syscall close() ==1809378== Warning: invalid file descriptor 1048567 in syscall close() ==1809378== Use --log-fd=<number> to select an alternative log fd. ==1809378== Warning: invalid file descriptor 1048568 in syscall close() ==1809378== Warning: invalid file descriptor 1048569 in syscall close() ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.4.0 "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 2012-2022, 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. 83775 grid points. 468381 volume elements. 2 surface markers. 17936 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 468381 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 24.283424 seconds on 1 core. ------------------------- Exit Success (SU2_DEF) ------------------------ /home/jenkins/util/SU2/SU2-v7.4.0/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 ==1813504== Warning: invalid file descriptor 1048564 in syscall close() ==1813504== Warning: invalid file descriptor 1048565 in syscall close() ==1813504== Warning: invalid file descriptor 1048566 in syscall close() ==1813504== Warning: invalid file descriptor 1048567 in syscall close() ==1813504== Use --log-fd=<number> to select an alternative log fd. ==1813504== Warning: invalid file descriptor 1048568 in syscall close() ==1813504== Warning: invalid file descriptor 1048569 in syscall close() ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.4.0 "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 2012-2022, 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. 83775 grid points. 468381 volume elements. 2 surface markers. 17936 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 468381 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: 20.6394. Standard deviation K: 49.3925. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 47.2388| 86.636| | CV Face Area Aspect Ratio| 1.07945| 107.626| | CV Sub-Volume Ratio| 1| 835.999| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 83775| 1/1.00| 10| | 1| 13821| 1/6.06| 8.22684| | 2| 2125| 1/6.5| 6.61095| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.53011 m^2, y-plane = 0.868549 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 +----------------------------------------------------------------------------------------------------------------------------------------------+ | 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| 3.0966e+00| -1.769868| 0.448506| 0.049654| 3.699238| -0.549589| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.0239e+00| -1.514606| 0.839346| 0.462880| 3.962010| -0.289362| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.0011e+00| -1.526763| 0.926179| 0.740347| 3.939565| 1.925842| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.9910e+00| -1.606192| 0.945796| 0.806951| 3.854348| -8.538088| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.9873e+00| -1.480946| 0.895276| 0.699471| 3.988747| -5.572881| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.48095| < -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 = 8970 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.249086e+09, tgt = 6.249086e+09, diff = 2.904410e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.101315e+09, tgt = 6.101315e+09, diff = 1.479870e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.122063e+07, tgt = 6.122063e+07, diff = 7.450581e-09 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.122314e+07, tgt = 6.122314e+07, diff = 0.000000e+00 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... ==1780741== ==1780741== HEAP SUMMARY: ==1780741== in use at exit: 4,334,065 bytes in 24,924 blocks ==1780741== total heap usage: 15,851,666 allocs, 15,826,742 frees, 113,061,338,678 bytes allocated ==1780741== ==1780741== LEAK SUMMARY: ==1780741== definitely lost: 0 bytes in 0 blocks ==1780741== indirectly lost: 0 bytes in 0 blocks ==1780741== possibly lost: 0 bytes in 0 blocks ==1780741== still reachable: 0 bytes in 0 blocks ==1780741== suppressed: 4,334,065 bytes in 24,924 blocks ==1780741== ==1780741== For lists of detected and suppressed errors, rerun with: -s ==1780741== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1907 from 1907) 1416.35user 18.43system 23:50.14elapsed 100%CPU (0avgtext+0avgdata 4493156maxresident)k 24inputs+333824outputs (0major+9828831minor)pagefaults 0swaps real 23m50.150s user 23m36.360s sys 0m18.467s + 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 ================================================= All tests pass! + exit 0 [GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.4/CAPS/training/LINUX64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.4,CAPS/training,LINUX64,reynolds) [Static Analysis] Using reference build 'ESP_ValgrindCaps/CASREV=7.4,ESPTEST=CAPS/training,ESP_ARCH=LINUX64,buildnode=reynolds #198' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_ValgrindCaps/CASREV=7.4,ESPTEST=CAPS/training,ESP_ARCH=LINUX64,buildnode=reynolds #200'. [Checks API] No suitable checks publisher found. [Valgrind] Files to copy: [Valgrind] Analysing valgrind results [Valgrind] Ending the valgrind analysis. [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: SUCCESS