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
==540989==
==540989== HEAP SUMMARY:
==540989== in use at exit: 4,228,451 bytes in 23,523 blocks
==540989== total heap usage: 21,557,252 allocs, 21,533,729 frees, 6,659,363,017 bytes allocated
==540989==
==540989== LEAK SUMMARY:
==540989== definitely lost: 0 bytes in 0 blocks
==540989== indirectly lost: 0 bytes in 0 blocks
==540989== possibly lost: 0 bytes in 0 blocks
==540989== still reachable: 0 bytes in 0 blocks
==540989== suppressed: 4,228,451 bytes in 23,523 blocks
==540989==
==540989== For lists of detected and suppressed errors, rerun with: -s
==540989== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
442.26user 2.44system 7:24.71elapsed 100%CPU (0avgtext+0avgdata 553144maxresident)k
8inputs+41112outputs (0major+1276092minor)pagefaults 0swaps
real 7m24.714s
user 7m22.265s
sys 0m2.454s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python tess_8_MeshSizing.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==576530== Memcheck, a memory error detector
==576530== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==576530== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==576530== Command: python tess_8_MeshSizing.py
==576530==
==> 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/7.6/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1655
Number of elements = 3225
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3225
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1655
Total number of elements = 3225
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - rootLeadingEdge
Mesh sizing name - wingSpar1
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 6587
Number of elements = 13200
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 13200
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 6587
Total number of elements = 13200
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - rootLeadingEdge
Mesh sizing name - wingSpar1
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 22190
Number of elements = 22191
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 22191
----------------------------
Total number of nodes = 22190
Total number of elements = 22191
==576530==
==576530== HEAP SUMMARY:
==576530== in use at exit: 4,228,451 bytes in 23,523 blocks
==576530== total heap usage: 23,593,618 allocs, 23,570,095 frees, 6,775,445,346 bytes allocated
==576530==
==576530== LEAK SUMMARY:
==576530== definitely lost: 0 bytes in 0 blocks
==576530== indirectly lost: 0 bytes in 0 blocks
==576530== possibly lost: 0 bytes in 0 blocks
==576530== still reachable: 0 bytes in 0 blocks
==576530== suppressed: 4,228,451 bytes in 23,523 blocks
==576530==
==576530== For lists of detected and suppressed errors, rerun with: -s
==576530== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
623.22user 4.22system 10:27.83elapsed 99%CPU (0avgtext+0avgdata 589524maxresident)k
8inputs+43920outputs (0major+1969794minor)pagefaults 0swaps
real 10m27.840s
user 10m23.230s
sys 0m4.228s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python tess_MinQuad.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==650341== Memcheck, a memory error detector
==650341== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==650341== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==650341== Command: python tess_MinQuad.py
==650341==
==> 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/7.6/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
==650341==
==650341== HEAP SUMMARY:
==650341== in use at exit: 4,228,195 bytes in 23,523 blocks
==650341== total heap usage: 16,314,395 allocs, 16,290,872 frees, 5,277,242,584 bytes allocated
==650341==
==650341== LEAK SUMMARY:
==650341== definitely lost: 0 bytes in 0 blocks
==650341== indirectly lost: 0 bytes in 0 blocks
==650341== possibly lost: 0 bytes in 0 blocks
==650341== still reachable: 0 bytes in 0 blocks
==650341== suppressed: 4,228,195 bytes in 23,523 blocks
==650341==
==650341== For lists of detected and suppressed errors, rerun with: -s
==650341== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1406 from 1406)
520.09user 3.75system 9:35.75elapsed 90%CPU (0avgtext+0avgdata 587484maxresident)k
8inputs+12680outputs (0major+1366569minor)pagefaults 0swaps
real 9m35.761s
user 8m40.102s
sys 0m3.753s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python tess_2k.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1011079== Memcheck, a memory error detector
==1011079== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1011079== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1011079== Command: python tess_2k.py
==1011079==
==> 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/7.6/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
==1011079==
==1011079== HEAP SUMMARY:
==1011079== in use at exit: 4,228,451 bytes in 23,523 blocks
==1011079== total heap usage: 18,104,574 allocs, 18,081,051 frees, 5,813,987,460 bytes allocated
==1011079==
==1011079== LEAK SUMMARY:
==1011079== definitely lost: 0 bytes in 0 blocks
==1011079== indirectly lost: 0 bytes in 0 blocks
==1011079== possibly lost: 0 bytes in 0 blocks
==1011079== still reachable: 0 bytes in 0 blocks
==1011079== suppressed: 4,228,451 bytes in 23,523 blocks
==1011079==
==1011079== For lists of detected and suppressed errors, rerun with: -s
==1011079== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
523.39user 3.29system 8:57.96elapsed 97%CPU (0avgtext+0avgdata 586932maxresident)k
8inputs+11384outputs (0major+1175881minor)pagefaults 0swaps
real 8m57.968s
user 8m43.395s
sys 0m3.297s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python astros_1_ModalClamped.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1224992== Memcheck, a memory error detector
==1224992== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1224992== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1224992== Command: python astros_1_ModalClamped.py
==1224992==
==> 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/7.6/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 235
Number of elements = 227
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 227
----------------------------
Total number of nodes = 235
Total number of elements = 227
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 0.0357647
2 : 0.102451
3 : 0.102451
4 : 0.159637
5 : 0.159637
6 : 0.215446
7 : 0.215446
8 : 0.350115
9 : 0.350115
10: 0.466966
==1224992==
==1224992== HEAP SUMMARY:
==1224992== in use at exit: 4,230,102 bytes in 23,527 blocks
==1224992== total heap usage: 17,811,460 allocs, 17,787,933 frees, 5,741,073,187 bytes allocated
==1224992==
==1224992== LEAK SUMMARY:
==1224992== definitely lost: 0 bytes in 0 blocks
==1224992== indirectly lost: 0 bytes in 0 blocks
==1224992== possibly lost: 0 bytes in 0 blocks
==1224992== still reachable: 0 bytes in 0 blocks
==1224992== suppressed: 4,230,102 bytes in 23,527 blocks
==1224992==
==1224992== For lists of detected and suppressed errors, rerun with: -s
==1224992== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
505.83user 3.38system 8:35.04elapsed 98%CPU (0avgtext+0avgdata 587568maxresident)k
24inputs+38688outputs (0major+1094687minor)pagefaults 0swaps
real 8m35.045s
user 8m25.835s
sys 0m3.389s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python astros_2_ModalSupport.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1307260== Memcheck, a memory error detector
==1307260== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1307260== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1307260== Command: python astros_2_ModalSupport.py
==1307260==
==> 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/7.6/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
==1307260==
==1307260== HEAP SUMMARY:
==1307260== in use at exit: 4,230,102 bytes in 23,527 blocks
==1307260== total heap usage: 17,809,375 allocs, 17,785,848 frees, 5,743,685,416 bytes allocated
==1307260==
==1307260== LEAK SUMMARY:
==1307260== definitely lost: 0 bytes in 0 blocks
==1307260== indirectly lost: 0 bytes in 0 blocks
==1307260== possibly lost: 0 bytes in 0 blocks
==1307260== still reachable: 0 bytes in 0 blocks
==1307260== suppressed: 4,230,102 bytes in 23,527 blocks
==1307260==
==1307260== For lists of detected and suppressed errors, rerun with: -s
==1307260== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
500.98user 3.08system 8:28.18elapsed 99%CPU (0avgtext+0avgdata 581876maxresident)k
19808inputs+40424outputs (93major+1012882minor)pagefaults 0swaps
real 8m28.187s
user 8m20.990s
sys 0m3.090s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python astros_3_StaticClamped.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1388919== Memcheck, a memory error detector
==1388919== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1388919== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1388919== Command: python astros_3_StaticClamped.py
==1388919==
==> 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/7.6/CAPS/training/LINUX64/CAPS/training/data/ESP/wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = wingSpar2, index = 1
Name = wingSpar1, index = 2
Name = rootLeadingEdge, index = 3
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 235
Number of elements = 227
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 227
----------------------------
Total number of nodes = 235
Total number of elements = 227
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
--> Maximum displacements:
--> Tmax 43461.879162311016
--> T1max 738.595
--> T2max 3686.25
--> T3max 43363.8
==1388919==
==1388919== HEAP SUMMARY:
==1388919== in use at exit: 4,230,102 bytes in 23,527 blocks
==1388919== total heap usage: 17,801,041 allocs, 17,777,514 frees, 5,676,882,803 bytes allocated
==1388919==
==1388919== LEAK SUMMARY:
==1388919== definitely lost: 0 bytes in 0 blocks
==1388919== indirectly lost: 0 bytes in 0 blocks
==1388919== possibly lost: 0 bytes in 0 blocks
==1388919== still reachable: 0 bytes in 0 blocks
==1388919== suppressed: 4,230,102 bytes in 23,527 blocks
==1388919==
==1388919== For lists of detected and suppressed errors, rerun with: -s
==1388919== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
468.00user 3.00system 7:58.90elapsed 98%CPU (0avgtext+0avgdata 560992maxresident)k
72048inputs+34656outputs (9major+917807minor)pagefaults 0swaps
real 7m58.909s
user 7m48.004s
sys 0m3.013s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python astros_4_Composite.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1472531== Memcheck, a memory error detector
==1472531== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1472531== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1472531== Command: python astros_4_Composite.py
==1472531==
==> 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/7.6/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
==1472531==
==1472531== HEAP SUMMARY:
==1472531== in use at exit: 4,230,102 bytes in 23,527 blocks
==1472531== total heap usage: 17,801,010 allocs, 17,777,483 frees, 5,692,447,771 bytes allocated
==1472531==
==1472531== LEAK SUMMARY:
==1472531== definitely lost: 0 bytes in 0 blocks
==1472531== indirectly lost: 0 bytes in 0 blocks
==1472531== possibly lost: 0 bytes in 0 blocks
==1472531== still reachable: 0 bytes in 0 blocks
==1472531== suppressed: 4,230,102 bytes in 23,527 blocks
==1472531==
==1472531== For lists of detected and suppressed errors, rerun with: -s
==1472531== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
459.43user 2.34system 7:54.82elapsed 97%CPU (0avgtext+0avgdata 565544maxresident)k
24inputs+34640outputs (0major+793126minor)pagefaults 0swaps
real 7m54.826s
user 7m39.436s
sys 0m2.351s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python nastran_5_Flutter.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1526718== Memcheck, a memory error detector
==1526718== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1526718== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1526718== Command: python nastran_5_Flutter.py
==1526718==
==> 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
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
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
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
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
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
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
==1526718==
==1526718== HEAP SUMMARY:
==1526718== in use at exit: 4,230,105 bytes in 23,527 blocks
==1526718== total heap usage: 14,854,028 allocs, 14,830,501 frees, 4,937,488,206 bytes allocated
==1526718==
==1526718== LEAK SUMMARY:
==1526718== definitely lost: 0 bytes in 0 blocks
==1526718== indirectly lost: 0 bytes in 0 blocks
==1526718== possibly lost: 0 bytes in 0 blocks
==1526718== still reachable: 0 bytes in 0 blocks
==1526718== suppressed: 4,230,105 bytes in 23,527 blocks
==1526718==
==1526718== For lists of detected and suppressed errors, rerun with: -s
==1526718== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1405 from 1405)
413.24user 2.52system 7:02.79elapsed 98%CPU (0avgtext+0avgdata 553340maxresident)k
4112inputs+13808outputs (7major+971902minor)pagefaults 0swaps
real 7m2.799s
user 6m53.244s
sys 0m2.532s
+ 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/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python aeroelastic_2_Iterative_SU2_Astros.py
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/training/LINUX64/CAPS/training/training.log
==1633837== Memcheck, a memory error detector
==1633837== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1633837== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1633837== Command: python aeroelastic_2_Iterative_SU2_Astros.py
==1633837==
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 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 07/25/23 @ 11:58AM
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 11.5.9
AFLR4 : Version Date 08/14/23 @ 12:27AM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 08/14/23 @ 01:20PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 6 Faces
EGADS : Body 0 has 10 Edges
EGADS : Body 0 has 6 Loops
EGADS : Body 0 has 6 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4
EGADS : 2 Yes 0 0 1 1 1 1 3 5
EGADS : 3 Yes 0 0 1 1 1 1 2
EGADS : 4 Yes 0 0 1 1 1 1 5 6
EGADS : 5 Yes 0 0 1 1 1 2 4 6
EGADS : 6 Yes 0 0 1 1 1 4 5
EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12
EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12
EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12
EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12
EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10
EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -3 5 1 -6
EGADS : 3 4 6
EGADS : 4 7 9 -8 -2
EGADS : 5 8 10 -7 -5
EGADS : 6 -9 -10
EGADS : 7 11 12 -13 -14
EGADS : 8 -15 18 17 -16
EGADS : 9 19 15 -20 -11
EGADS : 10 -21 13 22 -17
EGADS : 11 14 21 -18 -19
EGADS : 12 -12 20 16 -22
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 2 3 -4
EGADS : 2 Yes 1 -3 5 1 -6
EGADS : 3 Yes 1 4 6
EGADS : 4 Yes 1 7 9 -8 -2
EGADS : 5 Yes 1 8 10 -7 -5
EGADS : 6 Yes 1 -9 -10
EGADS : 7 Yes 1 11 12 -13 -14
EGADS : 8 Yes 1 -15 18 17 -16
EGADS : 9 Yes 1 19 15 -20 -11
EGADS : 10 Yes 1 -21 13 22 -17
EGADS : 11 Yes 1 14 21 -18 -19
EGADS : 12 Yes 1 -12 20 16 -22
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 1 3 1 1 4
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 5
EGADS : 6 0 Yes 4 2 1 2 3
EGADS : 7 0 Yes 1 5 1 4 5
EGADS : 8 0 Yes 3 6 1 4 5
EGADS : 9 0 Yes 5 6 1 4 6
EGADS : 10 0 Yes 6 5 1 5 6
EGADS : 11 1 Yes 8 7 NA 7 9
EGADS : 12 1 Yes 7 9 NA 7 12
EGADS : 13 1 Yes 10 9 NA 7 10
EGADS : 14 1 Yes 8 10 NA 7 11
EGADS : 15 1 Yes 12 11 NA 8 9
EGADS : 16 1 Yes 11 13 NA 8 12
EGADS : 17 1 Yes 14 13 NA 8 10
EGADS : 18 1 Yes 12 14 NA 8 11
EGADS : 19 1 Yes 8 12 NA 9 11
EGADS : 20 1 Yes 7 11 NA 9 12
EGADS : 21 1 Yes 10 14 NA 10 11
EGADS : 22 1 Yes 9 13 NA 10 12
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 1.61374306 0 0
EGADS : 2 Yes 2.37421202 0 0.355213563
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 1.40965066 0 0.270825378
EGADS : 5 Yes 2.37421202 3.87298335 0.355213563
EGADS : 6 Yes 1.40965066 3.87298335 0.270825378
EGADS : 7 Yes 0 0 77.6430368
EGADS : 8 Yes 0 0 0
EGADS : 9 Yes 0 77.4596689 77.6430368
EGADS : 10 Yes 0 77.4596689 0
EGADS : 11 Yes 78.6462641 0 77.6430368
EGADS : 12 Yes 78.6462641 0 0
EGADS : 13 Yes 78.6462641 77.4596689 77.6430368
EGADS : 14 Yes 78.6462641 77.4596689 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 154.919
AFLR4 : Min Bounding Box Length = 154.919
AFLR4 : Max Ref Bounding Box Length = 7.74597
AFLR4 : Min Ref Bounding Box Length = 0.433058
AFLR4 : Reference Length = 6.45497
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 21.0478
AFLR4 : Abs Min Surf Spacing = 0.0161374
AFLR4 : Min Surf Spacing = 0.0322749
AFLR4 : Max Surf Spacing = 0.645497
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : 8 CAD geometry 0 FARFIELD
AFLR4 : 9 CAD geometry 0 FARFIELD
AFLR4 : 10 CAD geometry 0 FARFIELD
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1658 3135 0
AFLR4 : Nodes, Trias,Quads= 971 1761 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1628 3077 0
AFLR4 : Nodes, Trias,Quads= 941 1703 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 48 65 0
AFLR4 : Nodes, Trias,Quads= 44 57 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1668 3155 0
AFLR4 : Nodes, Trias,Quads= 986 1791 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1625 3071 0
AFLR4 : Nodes, Trias,Quads= 930 1681 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 48 65 0
AFLR4 : Nodes, Trias,Quads= 44 57 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 3847 7686 938
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 3847 7686
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 3367 6423 0
AFLR4 : Nodes, Trias,Quads= 2401 4491 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 3394 6478 0
AFLR4 : Nodes, Trias,Quads= 2282 4254 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 145 226 0
AFLR4 : Nodes, Trias,Quads= 131 198 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 3366 6421 0
AFLR4 : Nodes, Trias,Quads= 2394 4477 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 3405 6500 0
AFLR4 : Nodes, Trias,Quads= 2289 4268 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 145 226 0
AFLR4 : Nodes, Trias,Quads= 131 198 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9265 18522 1526
OVERALL : CPU Time = 10.432 seconds
Body 1 (of 2)
Number of nodes = 8945
Number of elements = 17886
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 17886
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9265
Total number of elements = 18522
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 07/25/23 @ 11:58AM
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 11.5.9
AFLR4 : Version Date 08/14/23 @ 12:27AM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 08/14/23 @ 01:20PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 6 Faces
EGADS : Body 0 has 10 Edges
EGADS : Body 0 has 6 Loops
EGADS : Body 0 has 6 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4
EGADS : 2 Yes 0 0 1 1 1 1 3 5
EGADS : 3 Yes 0 0 1 1 1 1 2
EGADS : 4 Yes 0 0 1 1 1 1 5 6
EGADS : 5 Yes 0 0 1 1 1 2 4 6
EGADS : 6 Yes 0 0 1 1 1 4 5
EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12
EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12
EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12
EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12
EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10
EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -3 5 1 -6
EGADS : 3 4 6
EGADS : 4 7 9 -8 -2
EGADS : 5 8 10 -7 -5
EGADS : 6 -9 -10
EGADS : 7 11 12 -13 -14
EGADS : 8 -15 18 17 -16
EGADS : 9 19 15 -20 -11
EGADS : 10 -21 13 22 -17
EGADS : 11 14 21 -18 -19
EGADS : 12 -12 20 16 -22
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 2 3 -4
EGADS : 2 Yes 1 -3 5 1 -6
EGADS : 3 Yes 1 4 6
EGADS : 4 Yes 1 7 9 -8 -2
EGADS : 5 Yes 1 8 10 -7 -5
EGADS : 6 Yes 1 -9 -10
EGADS : 7 Yes 1 11 12 -13 -14
EGADS : 8 Yes 1 -15 18 17 -16
EGADS : 9 Yes 1 19 15 -20 -11
EGADS : 10 Yes 1 -21 13 22 -17
EGADS : 11 Yes 1 14 21 -18 -19
EGADS : 12 Yes 1 -12 20 16 -22
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 1 3 1 1 4
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 5
EGADS : 6 0 Yes 4 2 1 2 3
EGADS : 7 0 Yes 1 5 1 4 5
EGADS : 8 0 Yes 3 6 1 4 5
EGADS : 9 0 Yes 5 6 1 4 6
EGADS : 10 0 Yes 6 5 1 5 6
EGADS : 11 1 Yes 8 7 NA 7 9
EGADS : 12 1 Yes 7 9 NA 7 12
EGADS : 13 1 Yes 10 9 NA 7 10
EGADS : 14 1 Yes 8 10 NA 7 11
EGADS : 15 1 Yes 12 11 NA 8 9
EGADS : 16 1 Yes 11 13 NA 8 12
EGADS : 17 1 Yes 14 13 NA 8 10
EGADS : 18 1 Yes 12 14 NA 8 11
EGADS : 19 1 Yes 8 12 NA 9 11
EGADS : 20 1 Yes 7 11 NA 9 12
EGADS : 21 1 Yes 10 14 NA 10 11
EGADS : 22 1 Yes 9 13 NA 10 12
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 1.61374306 0 0
EGADS : 2 Yes 2.37421202 0 0.355213563
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 1.40965066 0 0.270825378
EGADS : 5 Yes 2.37421202 3.87298335 0.355213563
EGADS : 6 Yes 1.40965066 3.87298335 0.270825378
EGADS : 7 Yes 0 0 77.6430368
EGADS : 8 Yes 0 0 0
EGADS : 9 Yes 0 77.4596689 77.6430368
EGADS : 10 Yes 0 77.4596689 0
EGADS : 11 Yes 78.6462641 0 77.6430368
EGADS : 12 Yes 78.6462641 0 0
EGADS : 13 Yes 78.6462641 77.4596689 77.6430368
EGADS : 14 Yes 78.6462641 77.4596689 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
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 = 0.433058
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 16.9832
AFLR4 : Abs Min Surf Spacing = 0.00108265
AFLR4 : Min Surf Spacing = 0.00216529
AFLR4 : Max Surf Spacing = 0.0433058
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
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
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
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 18522
AFLR43 : Nodes = 9265
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 16.32.49
AFLR3 : Version Date 07/26/23 @ 12:32AM
AFLR3 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR3 : Compile Date 07/26/23 @ 01:49PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 9265 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 FarField
UG3 : 8 FarField
UG3 : 9 FarField
UG3 : 10 FarField
UG3 : 11 FarField
UG3 : 12 FarField
AFLR3 : CPU Time = 0.881 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 9265 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1854 12666
AFLR3 IG : Nodes, Elements = 3708 26130
AFLR3 IG : Nodes, Elements = 5562 39589
AFLR3 IG : Nodes, Elements = 7416 54244
AFLR3 IG : Nodes, Elements = 9270 69463
AFLR3 IG : Nodes, Elements = 9272 69530
AFLR3 IG : Nodes, Elements = 9272 69335
AFLR3 IG : Nodes, Elements = 9265 42285
AFLR3 IG : Nodes, Elements = 9265 42353
AFLR3 IG : Nodes, Elements = 9265 30496
AFLR3 IG : Nodes, Elements = 9265 28301
AFLR3 : CPU Time = 8.992 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 9265 28301
AFLR3 GG : Nodes, Elements = 13542 41195
AFLR3 GG : Nodes, Elements = 13542 58908
AFLR3 GG : Nodes, Elements = 13542 54250
AFLR3 GG : Nodes, Elements = 17058 65245
AFLR3 GG : Nodes, Elements = 17058 78728
AFLR3 GG : Nodes, Elements = 17058 74303
AFLR3 GG : Nodes, Elements = 20605 85295
AFLR3 GG : Nodes, Elements = 20605 99195
AFLR3 GG : Nodes, Elements = 20605 94904
AFLR3 GG : Nodes, Elements = 24311 106150
AFLR3 GG : Nodes, Elements = 24311 121010
AFLR3 GG : Nodes, Elements = 24311 116688
AFLR3 GG : Nodes, Elements = 28109 128222
AFLR3 GG : Nodes, Elements = 28109 143116
AFLR3 GG : Nodes, Elements = 28109 139085
AFLR3 GG : Nodes, Elements = 31833 150343
AFLR3 GG : Nodes, Elements = 31833 164956
AFLR3 GG : Nodes, Elements = 31833 161115
AFLR3 GG : Nodes, Elements = 35425 171944
AFLR3 GG : Nodes, Elements = 35425 186053
AFLR3 GG : Nodes, Elements = 35425 182380
AFLR3 GG : Nodes, Elements = 38915 192902
AFLR3 GG : Nodes, Elements = 38915 206546
AFLR3 GG : Nodes, Elements = 38915 203031
AFLR3 GG : Nodes, Elements = 42279 213161
AFLR3 GG : Nodes, Elements = 42279 226492
AFLR3 GG : Nodes, Elements = 42279 223051
AFLR3 GG : Nodes, Elements = 45563 232931
AFLR3 GG : Nodes, Elements = 45563 245768
AFLR3 GG : Nodes, Elements = 45563 242514
AFLR3 GG : Nodes, Elements = 48695 251935
AFLR3 GG : Nodes, Elements = 48695 264207
AFLR3 GG : Nodes, Elements = 48695 261088
AFLR3 GG : Nodes, Elements = 51591 269788
AFLR3 GG : Nodes, Elements = 51591 281183
AFLR3 GG : Nodes, Elements = 51591 278253
AFLR3 GG : Nodes, Elements = 54386 286650
AFLR3 GG : Nodes, Elements = 54386 297696
AFLR3 GG : Nodes, Elements = 54386 294892
AFLR3 GG : Nodes, Elements = 57084 303004
AFLR3 GG : Nodes, Elements = 57084 313644
AFLR3 GG : Nodes, Elements = 57084 310937
AFLR3 GG : Nodes, Elements = 59614 318534
AFLR3 GG : Nodes, Elements = 59614 328459
AFLR3 GG : Nodes, Elements = 59614 326028
AFLR3 GG : Nodes, Elements = 61932 332987
AFLR3 GG : Nodes, Elements = 61932 342053
AFLR3 GG : Nodes, Elements = 61932 339758
AFLR3 GG : Nodes, Elements = 64173 346486
AFLR3 GG : Nodes, Elements = 64173 355203
AFLR3 GG : Nodes, Elements = 64173 353091
AFLR3 GG : Nodes, Elements = 66220 359236
AFLR3 GG : Nodes, Elements = 66220 367234
AFLR3 GG : Nodes, Elements = 66220 365224
AFLR3 GG : Nodes, Elements = 68183 371120
AFLR3 GG : Nodes, Elements = 68183 378771
AFLR3 GG : Nodes, Elements = 68183 376893
AFLR3 GG : Nodes, Elements = 70021 382413
AFLR3 GG : Nodes, Elements = 70021 389635
AFLR3 GG : Nodes, Elements = 70021 387894
AFLR3 GG : Nodes, Elements = 71738 393050
AFLR3 GG : Nodes, Elements = 71738 399670
AFLR3 GG : Nodes, Elements = 71738 398113
AFLR3 GG : Nodes, Elements = 73289 402770
AFLR3 GG : Nodes, Elements = 73289 408828
AFLR3 GG : Nodes, Elements = 73289 407358
AFLR3 GG : Nodes, Elements = 74785 411846
AFLR3 GG : Nodes, Elements = 74785 417552
AFLR3 GG : Nodes, Elements = 74785 416226
AFLR3 GG : Nodes, Elements = 76147 420314
AFLR3 GG : Nodes, Elements = 76147 425638
AFLR3 GG : Nodes, Elements = 76147 424379
AFLR3 GG : Nodes, Elements = 77386 428096
AFLR3 GG : Nodes, Elements = 77386 432940
AFLR3 GG : Nodes, Elements = 77386 431774
AFLR3 GG : Nodes, Elements = 78483 435067
AFLR3 GG : Nodes, Elements = 78483 439378
AFLR3 GG : Nodes, Elements = 78483 438266
AFLR3 GG : Nodes, Elements = 79434 441119
AFLR3 GG : Nodes, Elements = 79434 444842
AFLR3 GG : Nodes, Elements = 79434 443913
AFLR3 GG : Nodes, Elements = 80223 446281
AFLR3 GG : Nodes, Elements = 80223 449423
AFLR3 GG : Nodes, Elements = 80223 448600
AFLR3 GG : Nodes, Elements = 80840 450451
AFLR3 GG : Nodes, Elements = 80840 452964
AFLR3 GG : Nodes, Elements = 80840 452292
AFLR3 GG : Nodes, Elements = 81284 453624
AFLR3 GG : Nodes, Elements = 81284 455393
AFLR3 GG : Nodes, Elements = 81284 454894
AFLR3 GG : Nodes, Elements = 81599 455839
AFLR3 GG : Nodes, Elements = 81599 457118
AFLR3 GG : Nodes, Elements = 81599 456750
AFLR3 GG : Nodes, Elements = 81779 457290
AFLR3 GG : Nodes, Elements = 81779 458010
AFLR3 GG : Nodes, Elements = 81779 457813
AFLR3 GG : Nodes, Elements = 81888 458140
AFLR3 GG : Nodes, Elements = 81888 458622
AFLR3 GG : Nodes, Elements = 81888 458452
AFLR3 GG : Nodes, Elements = 81937 458599
AFLR3 GG : Nodes, Elements = 81937 458810
AFLR3 GG : Nodes, Elements = 81937 458739
AFLR3 GG : Nodes, Elements = 81953 458787
AFLR3 GG : Nodes, Elements = 81953 458858
AFLR3 GG : Nodes, Elements = 81953 458828
AFLR3 GG : Nodes, Elements = 81961 458852
AFLR3 GG : Nodes, Elements = 81961 458887
AFLR3 GG : Nodes, Elements = 81961 458871
AFLR3 GG : Nodes, Elements = 81966 458886
AFLR3 GG : Nodes, Elements = 81966 458898
AFLR3 GG : Nodes, Elements = 81966 458893
AFLR3 GG : Nodes, Elements = 81968 458899
AFLR3 GG : Nodes, Elements = 81968 458905
AFLR3 GG : Nodes, Elements = 81968 458903
AFLR3 : CPU Time = 2.297 minutes
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 81968 458903
AFLR3 QI : Nodes, Elements = 81513 456317
AFLR3 QI : Nodes, Elements = 81426 455827
AFLR3 QI : Nodes, Elements = 81418 455777
AFLR3 QI : Nodes, Elements = 81416 455768
AFLR3 QI : Nodes, Elements = 81416 457723
AFLR3 QI : Nodes, Elements = 81416 455611
AFLR3 QI : Nodes, Elements = 81416 454711
AFLR3 QI : Nodes, Elements = 81416 454979
AFLR3 QI : Nodes, Elements = 81416 454537
AFLR3 QI : Nodes, Elements = 81416 454422
AFLR3 : CPU Time = 34.590 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 454422
UG3 : Min, Max Ang = 12.41 159.2
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 3.72e+06
UG3 : No. Tet Elems = 454422
UG3 : Min Vol = 1.01e-06
UG3 : Average Vol = 8.18
UG3 : Total-Tet-Vol = 3.72e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 454422
UG3 : Min, Max Q = 0.205 1
UG3 : Average Q = 0.896
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 3.147 minutes
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 454422
UG3 : Min, Max Ang = 12.41 159.2
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 3.72e+06
UG3 : No. Tet Elems = 454422
UG3 : Min Vol = 1.01e-06
UG3 : Average Vol = 8.18
UG3 : Total-Tet-Vol = 3.72e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 454422
UG3 : Min, Max Q = 0.361 1
UG3 : Average Q = 0.863
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
Volume mesh:
Number of nodes = 81416
Number of elements = 472944
Number of triangles = 18522
Number of quadrilatarals = 0
Number of tetrahedrals = 454422
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
/home/jenkins/util/SU2/SU2-v8.0.0/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-v8.0.0/bin/SU2/io/config.py:933: 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
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 10 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 7.74597 m.
Reference origin for moment evaluation is (0.322749, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
81416 grid points.
454422 volume elements.
2 surface markers.
17886 boundary elements in index 0 (Marker = BC_1).
636 boundary elements in index 1 (Marker = BC_2).
454422 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 3.71806e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 431.689. Mean K: 20.6913. Standard deviation K: 49.4454.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 51.1523| 86.7063|
| CV Face Area Aspect Ratio| 1.04012| 115.282|
| CV Sub-Volume Ratio| 1| 701.712|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 81416| 1/1.00| 10|
| 1| 13392| 1/6.08| 8.2187|
| 2| 2069| 1/6.47| 6.61504|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 20.5583 m^2.
Area projection in the x-plane = 1.52985 m^2, y-plane = 0.868532 m^2, z-plane = 9.83638 m^2.
Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m.
Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.0935e+00| -1.762880| 0.455100| 0.055818| 3.706226| -0.552238|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.0799e+00| -1.567620| 0.800265| 0.530357| 3.903824| -0.295493|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.1941e+00| -1.601362| 0.945584| 0.763508| 3.871421| 1.801614|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.1807e+00| -1.681553| 0.931856| 0.796718| 3.784455| -8.276542|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.2239e+00| -1.622632| 0.831000| 0.682309| 3.844421| -5.286333|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.62263| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticIterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file |surface_flow_aeroelasticIterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary |flow_aeroelasticIterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticIterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
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-v8.0.0/bin/SU2/run/interface.py:114: 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 = 16
Number of data points = 8945
CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
Rank 0: src = 6.247769e+09, tgt = 6.247769e+09, diff = 5.859232e-01
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 8945
CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
Rank 0: src = 6.100462e+09, tgt = 6.100462e+09, diff = 5.488014e-02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 8945
CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
Rank 0: src = 6.121567e+07, tgt = 6.121567e+07, diff = 1.005828e-06
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 8945
CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
Rank 0: src = 6.124703e+07, tgt = 6.124703e+07, diff = 1.490116e-08
Extracting external pressure loads from data transfer....
TransferName = upperWing
Number of Elements = 96 (total = 96)
Extracting external pressure loads from data transfer....
TransferName = lowerWing
Number of Elements = 96 (total = 192)
Extracting external pressure loads from data transfer....
TransferName = leftTip
Number of Elements = 10 (total = 202)
Extracting external pressure loads from data transfer....
TransferName = riteTip
Number of Elements = 10 (total = 212)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
Running mASTROS......
==> Running ASTROS post-analysis...
==> Running SU2 pre-analysis...
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
/home/jenkins/util/SU2/SU2-v8.0.0/bin/SU2/io/config.py:933: 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
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
81416 grid points.
454422 volume elements.
2 surface markers.
17886 boundary elements in index 0 (Marker = BC_1).
636 boundary elements in index 1 (Marker = BC_2).
454422 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 3.71806e+06.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 22.679953 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_0.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.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
/home/jenkins/util/SU2/SU2-v8.0.0/bin/SU2/run/interface.py:136: ResourceWarning: unclosed file <_io.BufferedReader name=4>
run_command(the_Command)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 10 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 7.74597 m.
Reference origin for moment evaluation is (0.322749, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
81416 grid points.
454422 volume elements.
2 surface markers.
17886 boundary elements in index 0 (Marker = BC_1).
636 boundary elements in index 1 (Marker = BC_2).
454422 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 206677 TETRAHEDRON volume elements.
There has been a re-orientation of 4617 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.44958e+17.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 2.87656. Mean K: 0.00648455. Standard deviation K: 0.0464997.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.137541| 84.713|
| CV Face Area Aspect Ratio| 1.95221| 1.70288e+06|
| CV Sub-Volume Ratio| 1| 4.01198e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 81416| 1/1.00| 10|
| 1| 13381| 1/6.08| 8.21645|
| 2| 2059| 1/6.5| 6.60437|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 82958.1 m.
Wetted area = 2.72489e+11 m^2.
Area projection in the x-plane = 1.26495e+11 m^2, y-plane = 4.14598e+10 m^2, z-plane = 2.88447e+09 m^2.
Max. coordinate in the x-direction = 3741.21 m, y-direction = 82958.1 m, z-direction = 0.13057 m.
Min. coordinate in the x-direction = -24654.1 m, y-direction = -120901 m, z-direction = -1.49006e+06 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.5205e+00| 11.162790| 14.130381| 14.018425| 16.631896| -0.040154|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.5360e+00| 11.290199| 14.034216| 13.933524| 16.745064| -0.034978|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.7154e+00| 11.451670| 14.100823| 13.982306| 16.865644| -0.040030|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.9154e+00| 11.520505| 14.157753| 14.065040| 16.980595| -0.032394|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.0127e+00| 11.581537| 14.205442| 14.102554| 17.047710| -0.043549|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 11.5815| < -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).
+-----------------------------------------------------------------------+
Warning: there are 2467 non-physical points in the solution.
Warning: 730 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
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 = 16
Number of data points = 8945
CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
Rank 0: src = 3.818419e+09, tgt = 3.818419e+09, diff = 1.426175e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 8945
CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
Rank 0: src = 3.521819e+09, tgt = 3.521818e+09, diff = 7.450709e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 8945
CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
Rank 0: src = 1.749554e+07, tgt = 1.749554e+07, diff = 0.000000e+00
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 8945
CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
Rank 0: src = 2.733346e+07, tgt = 2.733346e+07, diff = 0.000000e+00
Extracting external pressure loads from data transfer....
TransferName = upperWing
Number of Elements = 96 (total = 96)
Extracting external pressure loads from data transfer....
TransferName = lowerWing
Number of Elements = 96 (total = 192)
Extracting external pressure loads from data transfer....
TransferName = leftTip
Number of Elements = 10 (total = 202)
Extracting external pressure loads from data transfer....
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...
==1633837==
==1633837== HEAP SUMMARY:
==1633837== in use at exit: 4,455,522 bytes in 23,885 blocks
==1633837== total heap usage: 15,810,303 allocs, 15,786,418 frees, 111,162,284,896 bytes allocated
==1633837==
==1633837== LEAK SUMMARY:
==1633837== definitely lost: 0 bytes in 0 blocks
==1633837== indirectly lost: 0 bytes in 0 blocks
==1633837== possibly lost: 0 bytes in 0 blocks
==1633837== still reachable: 0 bytes in 0 blocks
==1633837== suppressed: 4,455,522 bytes in 23,885 blocks
==1633837==
==1633837== For lists of detected and suppressed errors, rerun with: -s
==1633837== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1429 from 1429)
2007.34user 37.40system 36:04.16elapsed 94%CPU (0avgtext+0avgdata 4358688maxresident)k
34736inputs+349184outputs (73major+10206289minor)pagefaults 0swaps
real 36m4.172s
user 33m27.355s
sys 0m37.447s
+ 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/7.6/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/7.6/CAPS/training/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/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/7.6/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/7.6/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/7.6/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] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[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=7.6,ESPTEST=CAPS/training,ESP_ARCH=LINUX64,buildnode=reynolds #216'.
[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
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