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Full LogInformation: 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 ---------------------------- Total number of nodes = 235 Total number of elements = 227 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 9 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 --> Eigen-frequencies: 1 : 0.0357647 2 : 0.102451 3 : 0.102451 4 : 0.159637 5 : 0.159637 6 : 0.215446 7 : 0.215446 8 : 0.350115 9 : 0.350115 real 0m25.912s user 0m27.303s sys 0m9.150s + 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/7.7/CAPS/training/DARWIN_ARM64/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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Name = ribSupport, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 Body 2 (of 2) Number of nodes = 1 Number of elements = 1 Number of node elements = 1 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 236 Total number of elements = 228 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = ribRootPoint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = ribRoot, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Name = ribSupport, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 236 Combined Number of elements = 228 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - leftWingSkin Property name - ribSupport Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribRootPoint No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribRootPoint No "groupName" specified for Support tuple ribRootPoint, going to use support name Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - ribRoot No "groupName" specified for Connection tuple ribRoot! Looking for automatic connections from the use of capsConnectLink for ribRoot 19 automatic connections were made for capsConnect ribRoot (node id 236) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing support cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 --> Eigen-frequencies: 1 : 0.0357647 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 0m21.035s user 0m26.649s sys 0m6.378s + 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/7.7/CAPS/training/DARWIN_ARM64/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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 ---------------------------- Total number of nodes = 235 Total number of elements = 227 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftPointLoad No "groupName" specified for Load tuple leftPointLoad, going to use load name Load name - ritePointLoad No "groupName" specified for Load tuple ritePointLoad, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG --> Maximum displacements: --> Tmax 43461.879162311016 --> T1max 738.595 --> T2max 3686.25 --> T3max 43363.8 real 0m14.909s user 0m23.073s sys 0m4.099s + 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/7.7/CAPS/training/DARWIN_ARM64/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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ==> Running ASTROS pre-analysis... ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 235 Number of elements = 227 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 227 ---------------------------- Total number of nodes = 235 Total number of elements = 227 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 235 Number of elements = 227 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 227 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 2 Load name - leftPointLoad No "groupName" specified for Load tuple leftPointLoad, going to use load name Load name - ritePointLoad No "groupName" specified for Load tuple ritePointLoad, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards ==> Running mASTROS... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG --> Maximum displacements: --> Tmax 12131.654370141774 --> T1max 275.241 --> T2max 1005.74 --> T3max 12103.5 real 0m15.147s user 0m22.845s sys 0m3.904s + 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/7.7/CAPS/training/DARWIN_ARM64/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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ==> Running Nastran pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Wing, index = 1 Name = wingSpar2, index = 2 Name = wingRib, index = 3 Name = riteWingSkin, index = 4 Name = wingSpar1, index = 5 Name = leftWingSkin, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 4) Getting surface mesh for body 2 (of 4) Getting surface mesh for body 3 (of 4) Getting surface mesh for body 4 (of 4) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 (of 4) Number of nodes = 11 Number of elements = 6 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 2 (of 4) Number of nodes = 11 Number of elements = 6 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 3 (of 4) Number of nodes = 11 Number of elements = 6 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 6 Body 4 (of 4) Number of nodes = 939 Number of elements = 1094 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 1094 ---------------------------- Total number of nodes = 972 Total number of elements = 1112 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Wing, index = 1 Name = wingSpar2, index = 2 Name = wingRib, index = 3 Name = riteWingSkin, index = 4 Name = wingSpar1, index = 5 Name = leftWingSkin, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 11 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 11 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 11 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Setting FEA Data Mesh for body = 3 Number of nodal coordinates = 939 Number of elements = 1094 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 1094 Combining multiple FEA meshes! Combined Number of nodal coordinates = 972 Combined Number of elements = 1112 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 1112 Getting vortex lattice surface data VLM surface name - upperWing Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 108 Surface 2: Number of points found for aero-spline = 108 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing Nastran instruction file.... Warning: No loads specified for case Flutter!!!! Writing aero card Writing analysis cards Writing constraint ADD cards Writing constraint cards Writing material cards Writing property cards Writing coordinate system cards Writing aeroelastic cards ==> Running Nastran... sh: nastran: command not found real 0m13.574s user 0m20.893s sys 0m4.404s + status=0 + set +x ================================================= data/session10/nastran_5_Flutter.py passed (as expected) ================================================= ================================================= aeroelastic_2_Iterative_SU2_Astros.py test; + python aeroelastic_2_Iterative_SU2_Astros.py + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) 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/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.7/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/bin/scribeWake.so' (no such file), '/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.3/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ==> Running SU2 pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Mesh sizing name - leftWing Mesh sizing name - riteWing Done getting mesh sizing parameters AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 arm64 AFLR2 : Compile Date 07/16/23 @ 01:42PM 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 11.5.8 AFLR4 : Version Date 07/24/23 @ 06:11PM AFLR4 : Compile OS Darwin 22.5.0 arm64 AFLR4 : Compile Date 07/24/23 @ 06:11PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 10 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 6 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 EGADS : 2 Yes 0 0 1 1 1 1 3 5 EGADS : 3 Yes 0 0 1 1 1 1 2 EGADS : 4 Yes 0 0 1 1 1 1 5 6 EGADS : 5 Yes 0 0 1 1 1 2 4 6 EGADS : 6 Yes 0 0 1 1 1 4 5 EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10 EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -3 5 1 -6 EGADS : 3 4 6 EGADS : 4 7 9 -8 -2 EGADS : 5 8 10 -7 -5 EGADS : 6 -9 -10 EGADS : 7 11 12 -13 -14 EGADS : 8 -15 18 17 -16 EGADS : 9 19 15 -20 -11 EGADS : 10 -21 13 22 -17 EGADS : 11 14 21 -18 -19 EGADS : 12 -12 20 16 -22 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 2 3 -4 EGADS : 2 Yes 1 -3 5 1 -6 EGADS : 3 Yes 1 4 6 EGADS : 4 Yes 1 7 9 -8 -2 EGADS : 5 Yes 1 8 10 -7 -5 EGADS : 6 Yes 1 -9 -10 EGADS : 7 Yes 1 11 12 -13 -14 EGADS : 8 Yes 1 -15 18 17 -16 EGADS : 9 Yes 1 19 15 -20 -11 EGADS : 10 Yes 1 -21 13 22 -17 EGADS : 11 Yes 1 14 21 -18 -19 EGADS : 12 Yes 1 -12 20 16 -22 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 2 EGADS : 2 0 Yes 1 3 1 1 4 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 5 EGADS : 6 0 Yes 4 2 1 2 3 EGADS : 7 0 Yes 1 5 1 4 5 EGADS : 8 0 Yes 3 6 1 4 5 EGADS : 9 0 Yes 5 6 1 4 6 EGADS : 10 0 Yes 6 5 1 5 6 EGADS : 11 1 Yes 8 7 NA 7 9 EGADS : 12 1 Yes 7 9 NA 7 12 EGADS : 13 1 Yes 10 9 NA 7 10 EGADS : 14 1 Yes 8 10 NA 7 11 EGADS : 15 1 Yes 12 11 NA 8 9 EGADS : 16 1 Yes 11 13 NA 8 12 EGADS : 17 1 Yes 14 13 NA 8 10 EGADS : 18 1 Yes 12 14 NA 8 11 EGADS : 19 1 Yes 8 12 NA 9 11 EGADS : 20 1 Yes 7 11 NA 9 12 EGADS : 21 1 Yes 10 14 NA 10 11 EGADS : 22 1 Yes 9 13 NA 10 12 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 1.61374306 0 0 EGADS : 2 Yes 2.37421202 0 0.355213563 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 1.40965066 0 0.270825378 EGADS : 5 Yes 2.37421202 3.87298335 0.355213563 EGADS : 6 Yes 1.40965066 3.87298335 0.270825378 EGADS : 7 Yes 0 0 77.6430368 EGADS : 8 Yes 0 0 0 EGADS : 9 Yes 0 77.4596689 77.6430368 EGADS : 10 Yes 0 77.4596689 0 EGADS : 11 Yes 78.6462641 0 77.6430368 EGADS : 12 Yes 78.6462641 0 0 EGADS : 13 Yes 78.6462641 77.4596689 77.6430368 EGADS : 14 Yes 78.6462641 77.4596689 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found 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 = 0.346 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 arm64 AFLR2 : Compile Date 07/16/23 @ 01:42PM 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 11.5.8 AFLR4 : Version Date 07/24/23 @ 06:11PM AFLR4 : Compile OS Darwin 22.5.0 arm64 AFLR4 : Compile Date 07/24/23 @ 06:11PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 10 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 6 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 EGADS : 2 Yes 0 0 1 1 1 1 3 5 EGADS : 3 Yes 0 0 1 1 1 1 2 EGADS : 4 Yes 0 0 1 1 1 1 5 6 EGADS : 5 Yes 0 0 1 1 1 2 4 6 EGADS : 6 Yes 0 0 1 1 1 4 5 EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10 EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -3 5 1 -6 EGADS : 3 4 6 EGADS : 4 7 9 -8 -2 EGADS : 5 8 10 -7 -5 EGADS : 6 -9 -10 EGADS : 7 11 12 -13 -14 EGADS : 8 -15 18 17 -16 EGADS : 9 19 15 -20 -11 EGADS : 10 -21 13 22 -17 EGADS : 11 14 21 -18 -19 EGADS : 12 -12 20 16 -22 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 2 3 -4 EGADS : 2 Yes 1 -3 5 1 -6 EGADS : 3 Yes 1 4 6 EGADS : 4 Yes 1 7 9 -8 -2 EGADS : 5 Yes 1 8 10 -7 -5 EGADS : 6 Yes 1 -9 -10 EGADS : 7 Yes 1 11 12 -13 -14 EGADS : 8 Yes 1 -15 18 17 -16 EGADS : 9 Yes 1 19 15 -20 -11 EGADS : 10 Yes 1 -21 13 22 -17 EGADS : 11 Yes 1 14 21 -18 -19 EGADS : 12 Yes 1 -12 20 16 -22 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 2 EGADS : 2 0 Yes 1 3 1 1 4 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 5 EGADS : 6 0 Yes 4 2 1 2 3 EGADS : 7 0 Yes 1 5 1 4 5 EGADS : 8 0 Yes 3 6 1 4 5 EGADS : 9 0 Yes 5 6 1 4 6 EGADS : 10 0 Yes 6 5 1 5 6 EGADS : 11 1 Yes 8 7 NA 7 9 EGADS : 12 1 Yes 7 9 NA 7 12 EGADS : 13 1 Yes 10 9 NA 7 10 EGADS : 14 1 Yes 8 10 NA 7 11 EGADS : 15 1 Yes 12 11 NA 8 9 EGADS : 16 1 Yes 11 13 NA 8 12 EGADS : 17 1 Yes 14 13 NA 8 10 EGADS : 18 1 Yes 12 14 NA 8 11 EGADS : 19 1 Yes 8 12 NA 9 11 EGADS : 20 1 Yes 7 11 NA 9 12 EGADS : 21 1 Yes 10 14 NA 10 11 EGADS : 22 1 Yes 9 13 NA 10 12 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 1.61374306 0 0 EGADS : 2 Yes 2.37421202 0 0.355213563 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 1.40965066 0 0.270825378 EGADS : 5 Yes 2.37421202 3.87298335 0.355213563 EGADS : 6 Yes 1.40965066 3.87298335 0.270825378 EGADS : 7 Yes 0 0 77.6430368 EGADS : 8 Yes 0 0 0 EGADS : 9 Yes 0 77.4596689 77.6430368 EGADS : 10 Yes 0 77.4596689 0 EGADS : 11 Yes 78.6462641 0 77.6430368 EGADS : 12 Yes 78.6462641 0 0 EGADS : 13 Yes 78.6462641 77.4596689 77.6430368 EGADS : 14 Yes 78.6462641 77.4596689 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found 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 22.6.0 arm64 AFLR3 : Compile Date 07/26/23 @ 12:37AM 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 = 0.028 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 9265 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1854 12671 AFLR3 IG : Nodes, Elements = 3708 26048 AFLR3 IG : Nodes, Elements = 5562 39573 AFLR3 IG : Nodes, Elements = 7416 54197 AFLR3 IG : Nodes, Elements = 9270 69488 AFLR3 IG : Nodes, Elements = 9272 69555 AFLR3 IG : Nodes, Elements = 9272 69365 AFLR3 IG : Nodes, Elements = 9265 42305 AFLR3 IG : Nodes, Elements = 9265 42377 AFLR3 IG : Nodes, Elements = 9265 30542 AFLR3 IG : Nodes, Elements = 9265 28159 AFLR3 : CPU Time = 0.216 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 9265 28159 AFLR3 GG : Nodes, Elements = 13573 41132 AFLR3 GG : Nodes, Elements = 13573 57791 AFLR3 GG : Nodes, Elements = 13573 53355 AFLR3 GG : Nodes, Elements = 17194 64584 AFLR3 GG : Nodes, Elements = 17194 78766 AFLR3 GG : Nodes, Elements = 17194 74338 AFLR3 GG : Nodes, Elements = 20911 85882 AFLR3 GG : Nodes, Elements = 20911 100467 AFLR3 GG : Nodes, Elements = 20911 96443 AFLR3 GG : Nodes, Elements = 24510 107410 AFLR3 GG : Nodes, Elements = 24510 121842 AFLR3 GG : Nodes, Elements = 24510 117785 AFLR3 GG : Nodes, Elements = 28166 128898 AFLR3 GG : Nodes, Elements = 28166 143103 AFLR3 GG : Nodes, Elements = 28166 139290 AFLR3 GG : Nodes, Elements = 31761 150166 AFLR3 GG : Nodes, Elements = 31761 164409 AFLR3 GG : Nodes, Elements = 31761 160645 AFLR3 GG : Nodes, Elements = 35289 171300 AFLR3 GG : Nodes, Elements = 35289 185209 AFLR3 GG : Nodes, Elements = 35289 181480 AFLR3 GG : Nodes, Elements = 38731 191856 AFLR3 GG : Nodes, Elements = 38731 205442 AFLR3 GG : Nodes, Elements = 38731 201972 AFLR3 GG : Nodes, Elements = 42032 211905 AFLR3 GG : Nodes, Elements = 42032 224908 AFLR3 GG : Nodes, Elements = 42032 221571 AFLR3 GG : Nodes, Elements = 45195 231090 AFLR3 GG : Nodes, Elements = 45195 243432 AFLR3 GG : Nodes, Elements = 45195 240288 AFLR3 GG : Nodes, Elements = 48245 249453 AFLR3 GG : Nodes, Elements = 48245 261471 AFLR3 GG : Nodes, Elements = 48245 258402 AFLR3 GG : Nodes, Elements = 51236 267395 AFLR3 GG : Nodes, Elements = 51236 279221 AFLR3 GG : Nodes, Elements = 51236 276130 AFLR3 GG : Nodes, Elements = 54029 284517 AFLR3 GG : Nodes, Elements = 54029 295376 AFLR3 GG : Nodes, Elements = 54029 292744 AFLR3 GG : Nodes, Elements = 56700 300769 AFLR3 GG : Nodes, Elements = 56700 311131 AFLR3 GG : Nodes, Elements = 56700 308540 AFLR3 GG : Nodes, Elements = 59242 316175 AFLR3 GG : Nodes, Elements = 59242 326210 AFLR3 GG : Nodes, Elements = 59242 323707 AFLR3 GG : Nodes, Elements = 61667 330993 AFLR3 GG : Nodes, Elements = 61667 340464 AFLR3 GG : Nodes, Elements = 61667 338120 AFLR3 GG : Nodes, Elements = 63935 344930 AFLR3 GG : Nodes, Elements = 63935 353875 AFLR3 GG : Nodes, Elements = 63935 351718 AFLR3 GG : Nodes, Elements = 66076 358149 AFLR3 GG : Nodes, Elements = 66076 366494 AFLR3 GG : Nodes, Elements = 66076 364423 AFLR3 GG : Nodes, Elements = 68042 370330 AFLR3 GG : Nodes, Elements = 68042 377955 AFLR3 GG : Nodes, Elements = 68042 376024 AFLR3 GG : Nodes, Elements = 69896 381591 AFLR3 GG : Nodes, Elements = 69896 388856 AFLR3 GG : Nodes, Elements = 69896 387110 AFLR3 GG : Nodes, Elements = 71648 392369 AFLR3 GG : Nodes, Elements = 71648 399197 AFLR3 GG : Nodes, Elements = 71648 397526 AFLR3 GG : Nodes, Elements = 73256 402350 AFLR3 GG : Nodes, Elements = 73256 408732 AFLR3 GG : Nodes, Elements = 73256 407090 AFLR3 GG : Nodes, Elements = 74761 411609 AFLR3 GG : Nodes, Elements = 74761 417497 AFLR3 GG : Nodes, Elements = 74761 416098 AFLR3 GG : Nodes, Elements = 76178 420352 AFLR3 GG : Nodes, Elements = 76178 425854 AFLR3 GG : Nodes, Elements = 76178 424496 AFLR3 GG : Nodes, Elements = 77453 428322 AFLR3 GG : Nodes, Elements = 77453 433381 AFLR3 GG : Nodes, Elements = 77453 432126 AFLR3 GG : Nodes, Elements = 78561 435451 AFLR3 GG : Nodes, Elements = 78561 439760 AFLR3 GG : Nodes, Elements = 78561 438675 AFLR3 GG : Nodes, Elements = 79504 441504 AFLR3 GG : Nodes, Elements = 79504 445258 AFLR3 GG : Nodes, Elements = 79504 444295 AFLR3 GG : Nodes, Elements = 80258 446558 AFLR3 GG : Nodes, Elements = 80258 449626 AFLR3 GG : Nodes, Elements = 80258 448802 AFLR3 GG : Nodes, Elements = 80867 450629 AFLR3 GG : Nodes, Elements = 80867 453103 AFLR3 GG : Nodes, Elements = 80867 452425 AFLR3 GG : Nodes, Elements = 81306 453742 AFLR3 GG : Nodes, Elements = 81306 455491 AFLR3 GG : Nodes, Elements = 81306 455046 AFLR3 GG : Nodes, Elements = 81644 456060 AFLR3 GG : Nodes, Elements = 81644 457414 AFLR3 GG : Nodes, Elements = 81644 457049 AFLR3 GG : Nodes, Elements = 81870 457727 AFLR3 GG : Nodes, Elements = 81870 458621 AFLR3 GG : Nodes, Elements = 81870 458386 AFLR3 GG : Nodes, Elements = 81989 458743 AFLR3 GG : Nodes, Elements = 81989 459233 AFLR3 GG : Nodes, Elements = 81989 459075 AFLR3 GG : Nodes, Elements = 82056 459276 AFLR3 GG : Nodes, Elements = 82056 459559 AFLR3 GG : Nodes, Elements = 82056 459463 AFLR3 GG : Nodes, Elements = 82086 459553 AFLR3 GG : Nodes, Elements = 82086 459667 AFLR3 GG : Nodes, Elements = 82086 459631 AFLR3 GG : Nodes, Elements = 82092 459649 AFLR3 GG : Nodes, Elements = 82092 459674 AFLR3 GG : Nodes, Elements = 82092 459663 AFLR3 GG : Nodes, Elements = 82093 459666 AFLR3 GG : Nodes, Elements = 82093 459669 AFLR3 GG : Nodes, Elements = 82093 459668 AFLR3 GG : Nodes, Elements = 82102 459695 AFLR3 GG : Nodes, Elements = 82102 459716 AFLR3 GG : Nodes, Elements = 82103 459719 AFLR3 GG : Nodes, Elements = 82103 459721 AFLR3 : CPU Time = 3.247 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 82103 459721 AFLR3 QI : Nodes, Elements = 81728 457610 AFLR3 QI : Nodes, Elements = 81700 457445 AFLR3 QI : Nodes, Elements = 81699 457439 AFLR3 QI : Nodes, Elements = 81699 459461 AFLR3 QI : Nodes, Elements = 81699 457335 AFLR3 QI : Nodes, Elements = 81699 456439 AFLR3 QI : Nodes, Elements = 81699 456666 AFLR3 QI : Nodes, Elements = 81699 456256 AFLR3 QI : Nodes, Elements = 81699 456168 AFLR3 : CPU Time = 0.667 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 456168 UG3 : Min, Max Ang = 11.21 153.1 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 = 456168 UG3 : Min Vol = 1.34e-06 UG3 : Average Vol = 8.15 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 = 456168 UG3 : Min, Max Q = 0.239 1 UG3 : Average Q = 0.897 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 4.273 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 456168 UG3 : Min, Max Ang = 11.21 153.1 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 = 456168 UG3 : Min Vol = 1.34e-06 UG3 : Average Vol = 8.15 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 = 456168 UG3 : Min, Max Q = 0.449 1 UG3 : Average Q = 0.874 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 2 : MAX XYZ DEVIATION 0.00136499 TOLERANCE 0.000320188 AT NODE 27 : INPUT EDGE COORDINATE T 0.999198 : INPUT X,Y,Z COORDINATES 0, 0, 0 : EVALUATED X,Y,Z COORDINATES -0.000353468, 8.07305e-20, 0.00131843 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 4 : MAX XYZ DEVIATION 0.00117205 TOLERANCE 0.000308776 AT NODE 31 : INPUT EDGE COORDINATE T 0.998842 : INPUT X,Y,Z COORDINATES 1.40965, -3.87298, 0.270825 : EVALUATED X,Y,Z COORDINATES 1.40946, -3.87298, 0.271982 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 : XYZ DEVIATION > TOLERANCE AT 26 NODES ON EDGE 5 : MAX XYZ DEVIATION 0.00129418 TOLERANCE 0.000381568 AT NODE 26 : INPUT EDGE COORDINATE T 0.999204 : INPUT X,Y,Z COORDINATES 1.61374, -3.22723e-33, -5.27047e-17 : EVALUATED X,Y,Z COORDINATES 1.61245, 4.41616e-21, 7.21214e-05 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 : XYZ DEVIATION > TOLERANCE AT 31 NODES ON EDGE 6 : MAX XYZ DEVIATION 0.00111832 TOLERANCE 0.000323207 AT NODE 31 : INPUT EDGE COORDINATE T 0.998871 : INPUT X,Y,Z COORDINATES 2.37421, -3.87298, 0.355214 : EVALUATED X,Y,Z COORDINATES 2.37312, -3.87298, 0.354979 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 9 : MAX XYZ DEVIATION 0.00117205 TOLERANCE 0.000308776 AT NODE 31 : INPUT EDGE COORDINATE T 0.998842 : INPUT X,Y,Z COORDINATES 1.40965, 3.87298, 0.270825 : EVALUATED X,Y,Z COORDINATES 1.40946, 3.87298, 0.271982 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 : XYZ DEVIATION > TOLERANCE AT 31 NODES ON EDGE 10 : MAX XYZ DEVIATION 0.00111832 TOLERANCE 0.000323207 AT NODE 31 : INPUT EDGE COORDINATE T 0.998871 : INPUT X,Y,Z COORDINATES 2.37421, 3.87298, 0.355214 : EVALUATED X,Y,Z COORDINATES 2.37312, 3.87298, 0.354979 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 *** NON-FATAL EGADS ERROR 3299 *** *** COORDINATES FOUND THAT DEVIATE FROM EGADS GEOMETRY *** 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 = 81699 Number of elements = 474690 Number of triangles = 18522 Number of quadrilatarals = 0 Number of tetrahedrals = 456168 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 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 10 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 7.74597 m. Reference origin for moment evaluation is (0.322749, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 81699 grid points. 456168 volume elements. 2 surface markers. 17886 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 456168 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: 20.6916. Standard deviation K: 49.4465. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 52.3268| 86.4922| | CV Face Area Aspect Ratio| 1.05921| 136.662| | CV Sub-Volume Ratio| 1| 1031.41| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 81699| 1/1.00| 10| | 1| 13482| 1/6.06| 8.22755| | 2| 2065| 1/6.53| 6.60314| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.52985 m^2, y-plane = 0.868532 m^2, z-plane = 9.83638 m^2. Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m. Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.2390e+00| -1.763634| 0.454346| 0.055065| 3.705472| -0.549813| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.2223e+00| -1.557227| 0.831900| 0.483309| 3.920639| -0.286468| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.1486e+00| -1.601882| 0.929231| 0.729303| 3.870045| 1.838064| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.1865e+00| -1.735361| 0.892372| 0.776808| 3.725077| -8.418444| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.1616e+00| -1.631750| 0.809611| 0.670969| 3.834332| -5.321841| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.63175| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 265 Number of elements = 346 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 346 ---------------------------- Total number of nodes = 265 Total number of elements = 346 Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = rootConstraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 2 Name = ritePointLoad, index = 1 Name = leftPointLoad, index = 2 Mapping capsBound attributes ................ Number of unique capsBound attributes = 4 Name = upperWing, index = 1 Name = lowerWing, index = 2 Name = leftTip, index = 3 Name = riteTip, index = 4 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 265 Number of elements = 346 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 346 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - leftWingSkin Property name - riteWingSkin Property name - wingRib Property name - wingSpar1 Property name - wingSpar2 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - rootConstraint No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - pressureAero No "groupName" specified for Load tuple pressureAero, going to use load name Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses CAPS Info: Reparameterization Bound -> upperWing -- nu, nv = 129 129 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.247260e+09, tgt = 6.247260e+09, diff = 3.352621e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.100815e+09, tgt = 6.100815e+09, diff = 4.194182e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.124019e+07, tgt = 6.124019e+07, diff = 7.450581e-09 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.123780e+07, tgt = 6.123780e+07, diff = 0.000000e+00 Extracting external pressure loads from data transfer.... TransferName = upperWing Number of Elements = 96 (total = 96) TransferName = lowerWing Number of Elements = 96 (total = 192) TransferName = leftTip Number of Elements = 10 (total = 202) TransferName = riteTip Number of Elements = 10 (total = 212) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards Running mASTROS...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ==> 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 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_0.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: aeroelasticIterative.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 81699 grid points. 456168 volume elements. 2 surface markers. 17886 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 456168 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 3.71806e+06. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). ----------------------- Write deformed grid files ----------------------- |SU2 mesh |aeroelasticIterative.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Solver Postprocessing ------------------------- Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. Completed in 26.609991 seconds on 1 core. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.5.1 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 10 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 7.74597 m. Reference origin for moment evaluation is (0.322749, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 81699 grid points. 456168 volume elements. 2 surface markers. 17886 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 456168 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: 20.6916. Standard deviation K: 49.4465. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 52.3268| 86.4922| | CV Face Area Aspect Ratio| 1.05921| 136.662| | CV Sub-Volume Ratio| 1| 1031.41| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 81699| 1/1.00| 10| | 1| 13482| 1/6.06| 8.22755| | 2| 2065| 1/6.53| 6.60314| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.52985 m^2, y-plane = 0.868532 m^2, z-plane = 9.83638 m^2. Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m. Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.2955e+00| -1.763634| 0.454346| 0.055065| 3.705472| -0.549813| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.1663e+00| -1.557227| 0.831900| 0.483309| 3.920639| -0.286468| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.1302e+00| -1.601882| 0.929231| 0.729303| 3.870045| 1.838064| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.1554e+00| -1.735361| 0.892372| 0.776808| 3.725077| -8.418444| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.1677e+00| -1.631750| 0.809611| 0.670969| 3.834332| -5.321841| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.63175| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.247260e+09, tgt = 6.247260e+09, diff = 3.352621e+01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.100815e+09, tgt = 6.100815e+09, diff = 4.194182e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.124019e+07, tgt = 6.124019e+07, diff = 7.450581e-09 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8945 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.123780e+07, tgt = 6.123780e+07, diff = 0.000000e+00 Extracting external pressure loads from data transfer.... TransferName = upperWing Number of Elements = 96 (total = 96) TransferName = lowerWing Number of Elements = 96 (total = 192) TransferName = leftTip Number of Elements = 10 (total = 202) TransferName = riteTip Number of Elements = 10 (total = 212) Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Writing coordinate system cards Running mASTROS...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ==> Running ASTROS post-analysis... real 3m38.829s user 3m34.766s sys 0m9.491s + 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 ================================================= All tests pass! ================================================= ================================================= [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/training/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.7,CAPS/training,DARWIN_ARM64,viggen) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/training,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #184' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/training,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #185'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS