Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = ritePointLoad, index = 1
Name = leftPointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = wingSpar2, index = 1
Name = wingRib, index = 2
Name = wingSpar1, index = 3
Name = leftWingSkin, index = 4
Name = riteWingSkin, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 235
Number of elements = 227
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 227
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 9
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
--> Eigen-frequencies:
1 : 0.0357647
2 : 0.102451
3 : 0.102451
4 : 0.159637
5 : 0.159637
6 : 0.215446
7 : 0.215446
8 : 0.350115
9 : 0.350115
real 0m34.775s
user 0m57.823s
sys 0m13.152s
+ status=0
+ set +x
=================================================
data/session10/astros_1_ModalClamped.py passed (as expected)
=================================================
=================================================
astros_2_ModalSupport.py test;
+ python astros_2_ModalSupport.py
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/training.log
==> Loading geometry from file "../ESP/wing3.csm"...
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/data/ESP/wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x7febc6864c54 for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7febc6864c54: note: pointer points here
ff ff ff ff 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x7feba683dca4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment
0x7feba683dca4: note: pointer points here
ec 12 f2 3f 94 a1 cb f7 0e f5 d2 3f 00 00 00 00 00 00 00 00 0c 00 00 00 99 99 e9 3f 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12 in
/Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x7febb688786c for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7febb688786c: note: pointer points here
e9 a7 d4 3f 00 00 00 00 00 00 00 00 00 00 00 00 04 00 00 00 00 00 00 00 00 00 00 00 ff ff ff ff
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x7febc740f0a4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment
0x7febc740f0a4: note: pointer points here
f6 60 bf bf 82 d2 5e 15 01 47 ca 3f 00 00 00 00 00 00 00 00 f4 ff ff ff 99 99 e9 3f 3f e1 af f4
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12 in
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 : 0.0357647
2 : 0.0365801
3 : 0.102451
4 : 0.102453
5 : 0.159637
6 : 0.1611
7 : 0.215446
8 : 0.215462
9 : 0.350115
10: 0.351196
real 0m30.509s
user 0m57.311s
sys 0m10.254s
+ status=0
+ set +x
=================================================
data/session10/astros_2_ModalSupport.py passed (as expected)
=================================================
=================================================
astros_3_StaticClamped.py test;
+ python astros_3_StaticClamped.py
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/training.log
==> Loading geometry from file "../ESP/wing3.csm"...
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/data/ESP/wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x7fc5e903a254 for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7fc5e903a254: note: pointer points here
ff ff ff ff 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 01 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x7fc5c90096a4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment
0x7fc5c90096a4: note: pointer points here
e9 a7 d4 3f a7 7b b6 f4 61 cf e8 3f 00 00 00 00 00 00 00 00 0c 00 00 00 99 99 e9 3f 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x7fc5f8c31aa4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment
0x7fc5f8c31aa4: note: pointer points here
f6 60 bf bf 82 d2 5e 15 01 47 ca 3f 00 00 00 00 00 00 00 00 f4 ff ff ff 99 99 e9 3f 3f e1 af f4
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12 in
/Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x7fc5f984b66c for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7fc5f984b66c: note: pointer points here
ec 12 f2 3f 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 ff ff ff ff
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in
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...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
--> Maximum displacements:
--> Tmax 43461.879162311016
--> T1max 738.595
--> T2max 3686.25
--> T3max 43363.8
real 0m24.687s
user 0m51.774s
sys 0m7.805s
+ status=0
+ set +x
=================================================
data/session10/astros_3_StaticClamped.py passed (as expected)
=================================================
=================================================
astros_4_Composite.py test;
+ python astros_4_Composite.py
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/training.log
==> Loading geometry from file "../ESP/wing3.csm"...
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
==> Running ASTROS pre-analysis...
ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/data/ESP/wing3.csm:104]]
SELECT specified nonexistant Edge
--> catching signal -223 (edge_not_found)
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x7fe667050054 for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7fe667050054: note: pointer points here
ff ff ff ff 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x7fe65681d2a4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment
0x7fe65681d2a4: note: pointer points here
e9 a7 d4 3f a7 7b b6 f4 61 cf e8 3f 00 00 00 00 00 00 00 00 0c 00 00 00 99 99 e9 3f 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12 in
/Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x7fe67746f26c for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7fe67746f26c: note: pointer points here
ac a5 c5 3f 00 00 00 00 00 00 00 00 00 00 00 00 04 00 00 00 00 00 00 00 00 00 00 00 ff ff ff ff
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x7fe64700a2a4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment
0x7fe64700a2a4: note: pointer points here
f6 60 bf bf 82 d2 5e 15 01 47 ca 3f 00 00 00 00 00 00 00 00 f4 ff ff ff 99 99 e9 3f 3f e1 af f4
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12 in
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...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
--> Maximum displacements:
--> Tmax 12131.654370141774
--> T1max 275.241
--> T2max 1005.74
--> T3max 12103.5
real 0m24.745s
user 0m52.701s
sys 0m7.321s
+ status=0
+ set +x
=================================================
data/session10/astros_4_Composite.py passed (as expected)
=================================================
=================================================
nastran_5_Flutter.py test;
+ python nastran_5_Flutter.py
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/training.log
==> Loading geometry from file "../ESP/wing3.csm"...
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
==> Running Nastran pre-analysis...
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x7f8393346254 for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7f8393346254: note: pointer points here
ff ff ff ff 69 0c 75 be c7 aa 87 c0 e2 fd ef 3f c7 aa 87 c0 e2 fd ef 3f 67 5d b4 e4 d1 5c 80 be
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in
/Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x7f839389726c for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7f839389726c: note: pointer points here
00 70 00 00 06 6d e6 bf 5d cd 57 14 ae ba 00 40 26 0d 91 2e 98 2a a3 3f a7 66 c7 2a ff ff ff ff
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x7f83933462a4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment
0x7f83933462a4: note: pointer points here
f7 7f 00 00 00 00 00 00 00 00 f0 3f d0 76 63 92 e2 fd ef 3f 0c 00 00 00 99 99 e9 3f 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x7f83938972a4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment
0x7f83938972a4: note: pointer points here
00 70 00 00 00 00 00 00 00 00 f0 3f d1 76 63 92 e2 fd ef 3f f4 ff ff ff 99 99 e9 3f 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12 in
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
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
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
Mass_Increment tuple is NULL - No mass increments 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 mass increment set
Writing Nastran instruction file....
Warning: No loads specified for case Flutter!!!!
Writing mass increment cards
Writing aero card
Writing analysis cards, 0
Writing constraint ADD cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Writing aeroelastic cards
Done writing aeroelastic cards
Done writing files
==> Running Nastran...
sh: nastran: command not found
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/data/session10/nastran_5_Flutter.py", line 138, in <module>
nastran.postAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis
self._analysisObj.postAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 2913, in postAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
nastranAIM.c:3039 in aimPostAnalysis():
Error: Unable to open file: nastran_modal.f06
================================================================================
real 0m24.342s
user 0m51.743s
sys 0m10.540s
+ status=1
+ set +x
=================================================
data/session10/nastran_5_Flutter.py failed (as NOT expected)
=================================================
=================================================
aeroelastic_2_Iterative_SU2_Astros.py test;
+ python aeroelastic_2_Iterative_SU2_Astros.py
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/CAPS/training/training.log
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
Information: Dynamic Loader for scribeWake.so not found
dlopen(scribeWake.so, 0x0082): tried: 'scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OSscribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/training/DARWIN64/ESP/DARWIN64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.8/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/15.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file)
==> Running SU2 pre-analysis...
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12: runtime error: reference binding to misaligned address 0x7fb36a09eaa4 for type 'value_type' (aka 'IntWalk_WalkingData'), which requires 8 byte alignment
0x7fb36a09eaa4: note: pointer points here
e9 a7 d4 3f 76 4e ac 27 7b cf e8 3f 00 00 00 00 00 00 00 00 0c 00 00 00 99 99 e9 3f 00 00 00 00
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1460:12 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64: runtime error: reference binding to misaligned address 0x7fb359907a54 for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7fb359907a54: note: pointer points here
ff ff ff ff 8c d4 d2 3f 7a 13 a0 fa 6c 47 d3 3f 8a 2b bc a6 4d ba d3 3f f9 f4 b0 7e 07 30 d4 3f
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/__iterator/reverse_iterator.h:145:64 in
/Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12: runtime error: reference binding to misaligned address 0x7fb349c2aea4 for type 'const value_type' (aka 'const IntWalk_WalkingData'), which requires 8 byte alignment
0x7fb349c2aea4: note: pointer points here
f6 60 bf bf 8a d0 ee 0c 89 45 ca 3f 00 00 00 00 00 00 00 00 f4 ff ff ff 99 99 e9 3f 00 65 48 a9
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Library/Developer/CommandLineTools/SDKs/MacOSX14.2.sdk/usr/include/c++/v1/vector:1470:12 in
/Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25: runtime error: constructor call on misaligned address 0x7fb36983386c for type 'IntWalk_WalkingData', which requires 8 byte alignment
0x7fb36983386c: note: pointer points here
ac a5 c5 3f 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 ff ff ff ff
^
SUMMARY: UndefinedBehaviorSanitizer: undefined-behavior /Users/jenkins/util/ESP/opencascade-7.8/trunk/src/NCollection/NCollection_OccAllocator.hxx:153:25 in
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 Darwin 22.5.0 x86_64
AFLR2 : Compile Date 07/25/23 @ 11:59AM
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 Darwin 22.5.0 x86_64
AFLR4 : Compile Date 08/14/23 @ 01:13PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
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 = 0.403 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 Darwin 22.5.0 x86_64
AFLR2 : Compile Date 07/25/23 @ 11:59AM
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 Darwin 22.5.0 x86_64
AFLR4 : Compile Date 08/14/23 @ 01:13PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
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 Darwin 22.5.0 x86_64
AFLR3 : Compile Date 07/26/23 @ 01:42PM
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 = 0.017 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 9265 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1854 12677
AFLR3 IG : Nodes, Elements = 3708 26008
AFLR3 IG : Nodes, Elements = 5562 39557
AFLR3 IG : Nodes, Elements = 7416 54153
AFLR3 IG : Nodes, Elements = 9270 69465
AFLR3 IG : Nodes, Elements = 9272 69530
AFLR3 IG : Nodes, Elements = 9272 69338
AFLR3 IG : Nodes, Elements = 9265 42283
AFLR3 IG : Nodes, Elements = 9265 42355
AFLR3 IG : Nodes, Elements = 9265 30583
AFLR3 IG : Nodes, Elements = 9265 28314
AFLR3 : CPU Time = 0.192 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 9265 28314
AFLR3 GG : Nodes, Elements = 13565 41265
AFLR3 GG : Nodes, Elements = 13565 58272
AFLR3 GG : Nodes, Elements = 13565 53767
AFLR3 GG : Nodes, Elements = 17175 64994
AFLR3 GG : Nodes, Elements = 17175 78903
AFLR3 GG : Nodes, Elements = 17175 74527
AFLR3 GG : Nodes, Elements = 20760 85673
AFLR3 GG : Nodes, Elements = 20760 99287
AFLR3 GG : Nodes, Elements = 20760 95369
AFLR3 GG : Nodes, Elements = 24435 106516
AFLR3 GG : Nodes, Elements = 24435 121184
AFLR3 GG : Nodes, Elements = 24435 117256
AFLR3 GG : Nodes, Elements = 28156 128573
AFLR3 GG : Nodes, Elements = 28156 142980
AFLR3 GG : Nodes, Elements = 28156 139177
AFLR3 GG : Nodes, Elements = 31795 150173
AFLR3 GG : Nodes, Elements = 31795 164442
AFLR3 GG : Nodes, Elements = 31795 160725
AFLR3 GG : Nodes, Elements = 35347 171457
AFLR3 GG : Nodes, Elements = 35347 185428
AFLR3 GG : Nodes, Elements = 35347 181759
AFLR3 GG : Nodes, Elements = 38762 192051
AFLR3 GG : Nodes, Elements = 38762 205381
AFLR3 GG : Nodes, Elements = 38762 202038
AFLR3 GG : Nodes, Elements = 42056 211952
AFLR3 GG : Nodes, Elements = 42056 224950
AFLR3 GG : Nodes, Elements = 42056 221626
AFLR3 GG : Nodes, Elements = 45234 231204
AFLR3 GG : Nodes, Elements = 45234 243657
AFLR3 GG : Nodes, Elements = 45234 240543
AFLR3 GG : Nodes, Elements = 48276 249687
AFLR3 GG : Nodes, Elements = 48276 261468
AFLR3 GG : Nodes, Elements = 48276 258572
AFLR3 GG : Nodes, Elements = 51189 267329
AFLR3 GG : Nodes, Elements = 51189 278669
AFLR3 GG : Nodes, Elements = 51189 275873
AFLR3 GG : Nodes, Elements = 53963 284210
AFLR3 GG : Nodes, Elements = 53963 295036
AFLR3 GG : Nodes, Elements = 53963 292368
AFLR3 GG : Nodes, Elements = 56598 300294
AFLR3 GG : Nodes, Elements = 56598 310651
AFLR3 GG : Nodes, Elements = 56598 308029
AFLR3 GG : Nodes, Elements = 59118 315597
AFLR3 GG : Nodes, Elements = 59118 325430
AFLR3 GG : Nodes, Elements = 59118 323021
AFLR3 GG : Nodes, Elements = 61449 330026
AFLR3 GG : Nodes, Elements = 61449 339172
AFLR3 GG : Nodes, Elements = 61449 336885
AFLR3 GG : Nodes, Elements = 63595 343330
AFLR3 GG : Nodes, Elements = 63595 351796
AFLR3 GG : Nodes, Elements = 63595 349708
AFLR3 GG : Nodes, Elements = 65633 355826
AFLR3 GG : Nodes, Elements = 65633 363777
AFLR3 GG : Nodes, Elements = 65633 361810
AFLR3 GG : Nodes, Elements = 67541 367536
AFLR3 GG : Nodes, Elements = 67541 375074
AFLR3 GG : Nodes, Elements = 67541 373136
AFLR3 GG : Nodes, Elements = 69307 378438
AFLR3 GG : Nodes, Elements = 69307 385478
AFLR3 GG : Nodes, Elements = 69307 383720
AFLR3 GG : Nodes, Elements = 70967 388704
AFLR3 GG : Nodes, Elements = 70967 395257
AFLR3 GG : Nodes, Elements = 70967 393596
AFLR3 GG : Nodes, Elements = 72531 398290
AFLR3 GG : Nodes, Elements = 72531 404309
AFLR3 GG : Nodes, Elements = 72531 402908
AFLR3 GG : Nodes, Elements = 73924 407091
AFLR3 GG : Nodes, Elements = 73924 412536
AFLR3 GG : Nodes, Elements = 73924 411179
AFLR3 GG : Nodes, Elements = 75267 415212
AFLR3 GG : Nodes, Elements = 75267 420511
AFLR3 GG : Nodes, Elements = 75267 419191
AFLR3 GG : Nodes, Elements = 76497 422884
AFLR3 GG : Nodes, Elements = 76497 427734
AFLR3 GG : Nodes, Elements = 76497 426524
AFLR3 GG : Nodes, Elements = 77644 429966
AFLR3 GG : Nodes, Elements = 77644 434393
AFLR3 GG : Nodes, Elements = 77644 433318
AFLR3 GG : Nodes, Elements = 78656 436355
AFLR3 GG : Nodes, Elements = 78656 440384
AFLR3 GG : Nodes, Elements = 78656 439388
AFLR3 GG : Nodes, Elements = 79544 442055
AFLR3 GG : Nodes, Elements = 79544 445638
AFLR3 GG : Nodes, Elements = 79544 444688
AFLR3 GG : Nodes, Elements = 80331 447049
AFLR3 GG : Nodes, Elements = 80331 450187
AFLR3 GG : Nodes, Elements = 80331 449370
AFLR3 GG : Nodes, Elements = 80931 451171
AFLR3 GG : Nodes, Elements = 80931 453580
AFLR3 GG : Nodes, Elements = 80931 452935
AFLR3 GG : Nodes, Elements = 81359 454219
AFLR3 GG : Nodes, Elements = 81359 456043
AFLR3 GG : Nodes, Elements = 81359 455506
AFLR3 GG : Nodes, Elements = 81657 456400
AFLR3 GG : Nodes, Elements = 81657 457662
AFLR3 GG : Nodes, Elements = 81657 457270
AFLR3 GG : Nodes, Elements = 81843 457828
AFLR3 GG : Nodes, Elements = 81843 458611
AFLR3 GG : Nodes, Elements = 81843 458362
AFLR3 GG : Nodes, Elements = 81935 458638
AFLR3 GG : Nodes, Elements = 81935 459025
AFLR3 GG : Nodes, Elements = 81935 458899
AFLR3 GG : Nodes, Elements = 81973 459013
AFLR3 GG : Nodes, Elements = 81973 459167
AFLR3 GG : Nodes, Elements = 81973 459119
AFLR3 GG : Nodes, Elements = 81985 459155
AFLR3 GG : Nodes, Elements = 81985 459199
AFLR3 GG : Nodes, Elements = 81985 459185
AFLR3 GG : Nodes, Elements = 81988 459194
AFLR3 GG : Nodes, Elements = 81988 459204
AFLR3 GG : Nodes, Elements = 81988 459201
AFLR3 GG : Nodes, Elements = 81991 459210
AFLR3 GG : Nodes, Elements = 81991 459216
AFLR3 : CPU Time = 2.748 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 81991 459216
AFLR3 QI : Nodes, Elements = 81614 457123
AFLR3 QI : Nodes, Elements = 81571 456885
AFLR3 QI : Nodes, Elements = 81567 456860
AFLR3 QI : Nodes, Elements = 81566 456855
AFLR3 QI : Nodes, Elements = 81566 458667
AFLR3 QI : Nodes, Elements = 81566 456715
AFLR3 QI : Nodes, Elements = 81566 455785
AFLR3 QI : Nodes, Elements = 81566 456021
AFLR3 QI : Nodes, Elements = 81566 455612
AFLR3 QI : Nodes, Elements = 81566 455498
AFLR3 : CPU Time = 0.696 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 455498
UG3 : Min, Max Ang = 12.26 152.3
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 3.72e+06
UG3 : No. Tet Elems = 455498
UG3 : Min Vol = 1.06e-06
UG3 : Average Vol = 8.16
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 = 455498
UG3 : Min, Max Q = 0.275 1
UG3 : Average Q = 0.896
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 3.753 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 455498
UG3 : Min, Max Ang = 12.26 152.3
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 3.72e+06
UG3 : No. Tet Elems = 455498
UG3 : Min Vol = 1.06e-06
UG3 : Average Vol = 8.16
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 = 455498
UG3 : Min, Max Q = 0.423 1
UG3 : Average Q = 0.869
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 7.8.0
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 = 81566
Number of elements = 474020
Number of triangles = 18522
Number of quadrilatarals = 0
Number of tetrahedrals = 455498
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......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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.
81566 grid points.
455498 volume elements.
2 surface markers.
17886 boundary elements in index 0 (Marker = BC_1).
636 boundary elements in index 1 (Marker = BC_2).
455498 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: 20.6912. Standard deviation K: 49.445.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 51.0154| 86.7993|
| CV Face Area Aspect Ratio| 1.05216| 152.584|
| CV Sub-Volume Ratio| 1| 921.642|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 81566| 1/1.00| 10|
| 1| 13476| 1/6.05| 8.2308|
| 2| 2091| 1/6.44| 6.63434|
+-------------------------------------------+
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| 1.8662e+00| -1.763280| 0.454700| 0.055418| 3.705826| -0.551636|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.8032e+00| -1.543005| 0.866397| 0.570888| 3.935591| -0.290232|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.7792e+00| -1.608388| 0.906939| 0.757061| 3.862340| 1.821947|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.7920e+00| -1.726813| 0.901646| 0.764205| 3.737590| -8.288684|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.7788e+00| -1.676212| 0.832255| 0.672807| 3.790259| -5.298930|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.67621| < -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) ------------------------
==> 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 = 6.249113e+09, tgt = 6.249113e+09, diff = 1.242791e+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 = 6.100904e+09, tgt = 6.100904e+09, diff = 3.147888e-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 = 6.121998e+07, tgt = 6.121998e+07, diff = 1.490116e-08
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 = 6.122522e+07, tgt = 6.122522e+07, diff = 7.450581e-09
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......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> 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......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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.
81566 grid points.
455498 volume elements.
2 surface markers.
17886 boundary elements in index 0 (Marker = BC_1).
636 boundary elements in index 1 (Marker = BC_2).
455498 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 16.736278 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) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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.
81566 grid points.
455498 volume elements.
2 surface markers.
17886 boundary elements in index 0 (Marker = BC_1).
636 boundary elements in index 1 (Marker = BC_2).
455498 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 211025 TETRAHEDRON volume elements.
There has been a re-orientation of 4591 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.42164e+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: 2.3744. Mean K: 0.00648893. Standard deviation K: 0.0433578.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.220086| 84.4018|
| CV Face Area Aspect Ratio| 1.66476| 1.62673e+06|
| CV Sub-Volume Ratio| 1| 1.75911e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 81566| 1/1.00| 10|
| 1| 13422| 1/6.08| 8.21979|
| 2| 2060| 1/6.52| 6.60139|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 80943.6 m.
Wetted area = 2.57049e+11 m^2.
Area projection in the x-plane = 1.15564e+11 m^2, y-plane = 3.58321e+10 m^2, z-plane = 2.9499e+09 m^2.
Max. coordinate in the x-direction = 3725.36 m, y-direction = 80943.6 m, z-direction = 0.130783 m.
Min. coordinate in the x-direction = -24366 m, y-direction = -117852 m, z-direction = -1.45123e+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| 1.9940e+00| 11.132660| 14.098618| 14.011400| 16.601765| 0.002565|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.9836e+00| 11.309200| 14.012144| 13.923169| 16.714478| 0.292164|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.9746e+00| 11.472718| 14.026537| 14.029632| 16.860018| 0.022794|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.9658e+00| 11.535230| 14.111362| 14.053715| 16.930954| -0.080127|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.9684e+00| 11.599883| 14.228092| 14.078245| 17.061880| 0.043370|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 11.5999| < -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 4249 non-physical points in the solution.
Warning: 1178 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 = 2.869462e+09, tgt = 2.869462e+09, diff = 6.422853e-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 = 3.010202e+09, tgt = 3.010202e+09, diff = 1.032414e+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 = 1.997963e+07, tgt = 1.997963e+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 = 2.421006e+07, tgt = 2.421006e+07, diff = 1.341105e-07
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......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running ASTROS post-analysis...
real 2m16.462s
user 2m40.810s
sys 0m12.261s
+ status=0
+ set +x
=================================================
data/session11/aeroelastic_2_Iterative_SU2_Astros.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
session07 pointwise
session08 fun3d
session11 fun3d+astros
=================================================
=================================================
Summary of examples NOT finished as expected
data/session10/nastran_5_Flutter.py
See training.log for more details.
=================================================
=================================================
=================================================
Build step 'Execute shell' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
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