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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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = riteWingSkin, index = 3 Name = wingSpar1, index = 4 Name = leftWingSkin, index = 5 Name = wingTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = leadingEdge, index = 3 Name = rootLeadingEdge, index = 4 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 299 Number of elements = 387 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 387 ---------------------------- Total number of nodes = 299 Total number of elements = 387 --> Total Elements 387 real 0m12.743s user 0m18.058s sys 0m4.179s + status=0 + set +x ================================================= solutions/session09/tess_MinQuad.py passed (as expected) ================================================= ================================================= tess_2k.py test; + python tess_2k.py + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/CAPS/training/training.log ==> Loading geometry from file "../../data/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/usr/local/lib/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache) ERROR:: (edge_not_found) in Branch Brch_000207 at [[/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/CAPS/training/data/ESP/wing3.csm:104]] SELECT specified nonexistant Edge --> catching signal -223 (edge_not_found) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = wingSpar2, index = 1 Name = wingRib, index = 2 Name = wingSpar1, index = 3 Name = leftWingSkin, index = 4 Name = riteWingSkin, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = wingSpar2, index = 1 Name = wingSpar1, index = 2 Name = rootLeadingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - rootLeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1289 Number of elements = 1189 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 1189 ---------------------------- Total number of nodes = 1289 Total number of elements = 1189 --> Total Elements 1189 real 0m13.720s user 0m18.200s sys 0m3.867s + status=0 + set +x ================================================= solutions/session09/tess_2k.py passed (as expected) ================================================= ================================================= astros_1_ModalClamped.py test; + python astros_1_ModalClamped.py + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/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 0m25.570s user 0m23.364s sys 0m9.658s + status=0 + set +x ================================================= data/session10/astros_1_ModalClamped.py passed (as expected) ================================================= ================================================= astros_2_ModalSupport.py test; + tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/CAPS/training/training.log + python astros_2_ModalSupport.py ==> 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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/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 0m20.697s user 0m22.811s sys 0m7.150s + 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/7.4/CAPS/training/DARWINM1/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/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 0m13.544s user 0m18.906s sys 0m4.369s + 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/7.4/CAPS/training/DARWINM1/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/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 0m13.829s user 0m18.686s sys 0m4.043s + 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/7.4/CAPS/training/DARWINM1/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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 0m16.112s user 0m18.336s sys 0m4.528s + 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/7.4/CAPS/training/DARWINM1/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1/ESP/DARWINM1/lib/scribeWake.so' (no such file), '/Users/jenkins/util/ESP/opencascade-7.4/trunk/build_undefined/install/./lib/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Users/jenkins/util/ESP/opencascade-7.4/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/14.0.0/lib/darwin/scribeWake.so' (no such file), '/System/Volumes/Preboot/Cryptexes/OS/Library/Developer/CommandLineTools/usr/lib/clang/14.0.0/lib/darwin/scribeWake.so' (no such file), '/usr/lib/scribeWake.so' (no such file, not in dyld cache), 'scribeWake.so' (no such file), '/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 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Darwin 22.3.0 arm64 AFLR2 : Compile Date 03/08/23 @ 05:04PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.3.17 AFLR4 : Version Date 03/03/23 @ 03:12PM AFLR4 : Compile OS Darwin 22.3.0 arm64 AFLR4 : Compile Date 03/08/23 @ 05:05PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 10 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 6 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 EGADS : 2 Yes 0 0 1 1 1 1 3 5 EGADS : 3 Yes 0 0 1 1 1 1 2 EGADS : 4 Yes 0 0 1 1 1 1 5 6 EGADS : 5 Yes 0 0 1 1 1 2 4 6 EGADS : 6 Yes 0 0 1 1 1 4 5 EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10 EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 3 -4 EGADS : 2 -3 5 1 -6 EGADS : 3 4 6 EGADS : 4 7 9 -8 -2 EGADS : 5 8 10 -7 -5 EGADS : 6 -9 -10 EGADS : 7 11 12 -13 -14 EGADS : 8 -15 18 17 -16 EGADS : 9 19 15 -20 -11 EGADS : 10 -21 13 22 -17 EGADS : 11 14 21 -18 -19 EGADS : 12 -12 20 16 -22 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 2 3 -4 EGADS : 2 Yes 1 -3 5 1 -6 EGADS : 3 Yes 1 4 6 EGADS : 4 Yes 1 7 9 -8 -2 EGADS : 5 Yes 1 8 10 -7 -5 EGADS : 6 Yes 1 -9 -10 EGADS : 7 Yes 1 11 12 -13 -14 EGADS : 8 Yes 1 -15 18 17 -16 EGADS : 9 Yes 1 19 15 -20 -11 EGADS : 10 Yes 1 -21 13 22 -17 EGADS : 11 Yes 1 14 21 -18 -19 EGADS : 12 Yes 1 -12 20 16 -22 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 2 EGADS : 2 0 Yes 1 3 1 1 4 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 3 EGADS : 5 0 Yes 3 1 1 2 5 EGADS : 6 0 Yes 4 2 1 2 3 EGADS : 7 0 Yes 1 5 1 4 5 EGADS : 8 0 Yes 3 6 1 4 5 EGADS : 9 0 Yes 5 6 1 4 6 EGADS : 10 0 Yes 6 5 1 5 6 EGADS : 11 1 Yes 8 7 NA 7 9 EGADS : 12 1 Yes 7 9 NA 7 12 EGADS : 13 1 Yes 10 9 NA 7 10 EGADS : 14 1 Yes 8 10 NA 7 11 EGADS : 15 1 Yes 12 11 NA 8 9 EGADS : 16 1 Yes 11 13 NA 8 12 EGADS : 17 1 Yes 14 13 NA 8 10 EGADS : 18 1 Yes 12 14 NA 8 11 EGADS : 19 1 Yes 8 12 NA 9 11 EGADS : 20 1 Yes 7 11 NA 9 12 EGADS : 21 1 Yes 10 14 NA 10 11 EGADS : 22 1 Yes 9 13 NA 10 12 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 1.61374306 0 0 EGADS : 2 Yes 2.37421202 0 0.355213563 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 1.40965066 0 0.270825378 EGADS : 5 Yes 2.37421202 3.87298335 0.355213563 EGADS : 6 Yes 1.40965066 3.87298335 0.270825378 EGADS : 7 Yes 0 0 77.6430368 EGADS : 8 Yes 0 0 0 EGADS : 9 Yes 0 77.4596689 77.6430368 EGADS : 10 Yes 0 77.4596689 0 EGADS : 11 Yes 78.6462641 0 77.6430368 EGADS : 12 Yes 78.6462641 0 0 EGADS : 13 Yes 78.6462641 77.4596689 77.6430368 EGADS : 14 Yes 78.6462641 77.4596689 0 AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 154.919 AFLR4 : Min Bounding Box Length = 154.919 AFLR4 : Max Ref Bounding Box Length = 7.74597 AFLR4 : Min Ref Bounding Box Length = 0.433058 AFLR4 : Reference Length = 6.45497 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 21.0478 AFLR4 : Abs Min Surf Spacing = 0.0161374 AFLR4 : Min Surf Spacing = 0.0322749 AFLR4 : Max Surf Spacing = 0.645497 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : 10 CAD geometry 0 FARFIELD AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 1658 3135 0 AFLR4 : Nodes, Trias,Quads= 971 1761 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 1628 3077 0 AFLR4 : Nodes, Trias,Quads= 941 1703 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 48 65 0 AFLR4 : Nodes, Trias,Quads= 44 57 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1668 3155 0 AFLR4 : Nodes, Trias,Quads= 986 1791 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 1625 3071 0 AFLR4 : Nodes, Trias,Quads= 930 1681 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 48 65 0 AFLR4 : Nodes, Trias,Quads= 44 57 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 3847 7686 938 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 3847 7686 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 6118 11925 0 AFLR4 : Nodes, Trias,Quads= 2408 4505 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 5960 11610 0 AFLR4 : Nodes, Trias,Quads= 2296 4282 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 147 230 0 AFLR4 : Nodes, Trias,Quads= 131 198 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 6173 12035 0 AFLR4 : Nodes, Trias,Quads= 2395 4479 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 6053 11796 0 AFLR4 : Nodes, Trias,Quads= 2292 4274 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 147 230 0 AFLR4 : Nodes, Trias,Quads= 131 198 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 73 116 0 AFLR4 : Nodes, Trias,Quads= 68 106 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9290 18572 1526 OVERALL : CPU Time = 0.701 seconds Body 1 (of 2) Number of nodes = 8970 Number of elements = 17936 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 17936 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 320 Number of elements = 636 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 636 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9290 Total number of elements = 18572 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = leftWing, index = 1 Name = riteWing, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Farfield, index = 2 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.6 AFLR2 : Version Date 11/20/22 @ 09:21PM AFLR2 : Compile OS Darwin 22.3.0 arm64 AFLR2 : Compile Date 03/08/23 @ 05:04PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.3.17 AFLR4 : Version Date 03/03/23 @ 03:12PM AFLR4 : Compile OS Darwin 22.3.0 arm64 AFLR4 : Compile Date 03/08/23 @ 05:05PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 EGADS : --------------------------------------- DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 9290 18572 1526 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.39 AFLR3 : Version Date 03/10/23 @ 04:32PM AFLR3 : Compile OS Darwin 22.3.0 arm64 AFLR3 : Compile Date 03/10/23 @ 04:32PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 9290 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 FarField UG3 : 8 FarField UG3 : 9 FarField UG3 : 10 FarField UG3 : 11 FarField UG3 : 12 FarField AFLR3 : CPU Time = 0.028 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 9290 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1860 12700 AFLR3 IG : Nodes, Elements = 3720 25924 AFLR3 IG : Nodes, Elements = 5580 39649 AFLR3 IG : Nodes, Elements = 7440 54287 AFLR3 IG : Nodes, Elements = 9297 69664 AFLR3 IG : Nodes, Elements = 9297 69489 AFLR3 IG : Nodes, Elements = 9290 42433 AFLR3 IG : Nodes, Elements = 9290 42497 AFLR3 IG : Nodes, Elements = 9290 30841 AFLR3 IG : Nodes, Elements = 9290 28702 AFLR3 : CPU Time = 0.412 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 9290 28702 AFLR3 GG : Nodes, Elements = 13555 41560 AFLR3 GG : Nodes, Elements = 13555 58080 AFLR3 GG : Nodes, Elements = 13555 53524 AFLR3 GG : Nodes, Elements = 17228 64981 AFLR3 GG : Nodes, Elements = 17228 79255 AFLR3 GG : Nodes, Elements = 17228 74661 AFLR3 GG : Nodes, Elements = 20849 85853 AFLR3 GG : Nodes, Elements = 20849 99995 AFLR3 GG : Nodes, Elements = 20849 95874 AFLR3 GG : Nodes, Elements = 24662 107400 AFLR3 GG : Nodes, Elements = 24662 122576 AFLR3 GG : Nodes, Elements = 24662 118534 AFLR3 GG : Nodes, Elements = 28461 130019 AFLR3 GG : Nodes, Elements = 28461 144891 AFLR3 GG : Nodes, Elements = 28461 141008 AFLR3 GG : Nodes, Elements = 32128 152066 AFLR3 GG : Nodes, Elements = 32128 166319 AFLR3 GG : Nodes, Elements = 32128 162608 AFLR3 GG : Nodes, Elements = 35701 173394 AFLR3 GG : Nodes, Elements = 35701 187491 AFLR3 GG : Nodes, Elements = 35701 183901 AFLR3 GG : Nodes, Elements = 39142 194279 AFLR3 GG : Nodes, Elements = 39142 207884 AFLR3 GG : Nodes, Elements = 39142 204414 AFLR3 GG : Nodes, Elements = 42473 214446 AFLR3 GG : Nodes, Elements = 42473 227388 AFLR3 GG : Nodes, Elements = 42473 224083 AFLR3 GG : Nodes, Elements = 45669 233700 AFLR3 GG : Nodes, Elements = 45669 246187 AFLR3 GG : Nodes, Elements = 45669 243070 AFLR3 GG : Nodes, Elements = 48731 252281 AFLR3 GG : Nodes, Elements = 48731 264213 AFLR3 GG : Nodes, Elements = 48731 261246 AFLR3 GG : Nodes, Elements = 51644 270009 AFLR3 GG : Nodes, Elements = 51644 281314 AFLR3 GG : Nodes, Elements = 51644 278514 AFLR3 GG : Nodes, Elements = 54396 286787 AFLR3 GG : Nodes, Elements = 54396 297481 AFLR3 GG : Nodes, Elements = 54396 294905 AFLR3 GG : Nodes, Elements = 56974 302649 AFLR3 GG : Nodes, Elements = 56974 312700 AFLR3 GG : Nodes, Elements = 56974 310229 AFLR3 GG : Nodes, Elements = 59377 317447 AFLR3 GG : Nodes, Elements = 59377 326833 AFLR3 GG : Nodes, Elements = 59377 324465 AFLR3 GG : Nodes, Elements = 61675 331370 AFLR3 GG : Nodes, Elements = 61675 340319 AFLR3 GG : Nodes, Elements = 61675 338141 AFLR3 GG : Nodes, Elements = 63805 344539 AFLR3 GG : Nodes, Elements = 63805 352968 AFLR3 GG : Nodes, Elements = 63805 350870 AFLR3 GG : Nodes, Elements = 65799 356855 AFLR3 GG : Nodes, Elements = 65799 364645 AFLR3 GG : Nodes, Elements = 65799 362734 AFLR3 GG : Nodes, Elements = 67646 368283 AFLR3 GG : Nodes, Elements = 67646 375504 AFLR3 GG : Nodes, Elements = 67646 373675 AFLR3 GG : Nodes, Elements = 69384 378893 AFLR3 GG : Nodes, Elements = 69384 385704 AFLR3 GG : Nodes, Elements = 69384 383992 AFLR3 GG : Nodes, Elements = 71029 388932 AFLR3 GG : Nodes, Elements = 71029 395368 AFLR3 GG : Nodes, Elements = 71029 393789 AFLR3 GG : Nodes, Elements = 72564 398397 AFLR3 GG : Nodes, Elements = 72564 404327 AFLR3 GG : Nodes, Elements = 72564 402921 AFLR3 GG : Nodes, Elements = 73981 407174 AFLR3 GG : Nodes, Elements = 73981 412757 AFLR3 GG : Nodes, Elements = 73981 411348 AFLR3 GG : Nodes, Elements = 75283 415256 AFLR3 GG : Nodes, Elements = 75283 420354 AFLR3 GG : Nodes, Elements = 75283 419109 AFLR3 GG : Nodes, Elements = 76464 422658 AFLR3 GG : Nodes, Elements = 76464 427351 AFLR3 GG : Nodes, Elements = 76464 426188 AFLR3 GG : Nodes, Elements = 77539 429416 AFLR3 GG : Nodes, Elements = 77539 433574 AFLR3 GG : Nodes, Elements = 77539 432568 AFLR3 GG : Nodes, Elements = 78412 435189 AFLR3 GG : Nodes, Elements = 78412 438693 AFLR3 GG : Nodes, Elements = 78412 437768 AFLR3 GG : Nodes, Elements = 79113 439872 AFLR3 GG : Nodes, Elements = 79113 442688 AFLR3 GG : Nodes, Elements = 79113 441883 AFLR3 GG : Nodes, Elements = 79672 443561 AFLR3 GG : Nodes, Elements = 79672 445800 AFLR3 GG : Nodes, Elements = 79672 445210 AFLR3 GG : Nodes, Elements = 80049 446341 AFLR3 GG : Nodes, Elements = 80049 447894 AFLR3 GG : Nodes, Elements = 80049 447435 AFLR3 GG : Nodes, Elements = 80324 448260 AFLR3 GG : Nodes, Elements = 80324 449380 AFLR3 GG : Nodes, Elements = 80324 449066 AFLR3 GG : Nodes, Elements = 80444 449426 AFLR3 GG : Nodes, Elements = 80444 449915 AFLR3 GG : Nodes, Elements = 80444 449756 AFLR3 GG : Nodes, Elements = 80499 449922 AFLR3 GG : Nodes, Elements = 80499 450134 AFLR3 GG : Nodes, Elements = 80499 450073 AFLR3 GG : Nodes, Elements = 80522 450142 AFLR3 GG : Nodes, Elements = 80522 450237 AFLR3 GG : Nodes, Elements = 80522 450203 AFLR3 GG : Nodes, Elements = 80529 450224 AFLR3 GG : Nodes, Elements = 80529 450258 AFLR3 GG : Nodes, Elements = 80529 450241 AFLR3 GG : Nodes, Elements = 80531 450247 AFLR3 GG : Nodes, Elements = 80531 450255 AFLR3 GG : Nodes, Elements = 80531 450253 AFLR3 GG : Nodes, Elements = 80538 450274 AFLR3 GG : Nodes, Elements = 80538 450288 AFLR3 GG : Nodes, Elements = 80538 450286 AFLR3 : CPU Time = 4.298 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 80538 450286 AFLR3 QI : Nodes, Elements = 80147 448095 AFLR3 QI : Nodes, Elements = 80101 447827 AFLR3 QI : Nodes, Elements = 80092 447775 AFLR3 QI : Nodes, Elements = 80092 449779 AFLR3 QI : Nodes, Elements = 80092 447675 AFLR3 QI : Nodes, Elements = 80092 446779 AFLR3 QI : Nodes, Elements = 80092 447083 AFLR3 QI : Nodes, Elements = 80092 446639 AFLR3 QI : Nodes, Elements = 80092 446543 AFLR3 : CPU Time = 0.638 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 446543 UG3 : Min, Max Ang = 10.97 156 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 = 446543 UG3 : Min Vol = 1.05e-06 UG3 : Average Vol = 8.33 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 = 446543 UG3 : Min, Max Q = 0.221 1 UG3 : Average Q = 0.896 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 5.484 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 446543 UG3 : Min, Max Ang = 10.97 156 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 = 446543 UG3 : Min Vol = 1.05e-06 UG3 : Average Vol = 8.33 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 = 446543 UG3 : Min, Max Q = 0.356 1 UG3 : Average Q = 0.863 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 EGADS : --------------------------------------- EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 13 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 14 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 15 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 7 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 8 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12 EGADS : EGADS TESS CREATED EGADS : CHECK TESS GLOBAL FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 7 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 8 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12 Volume mesh: Number of nodes = 80092 Number of elements = 465115 Number of triangles = 18572 Number of quadrilatarals = 0 Number of tetrahedrals = 446543 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing Done getting CFD boundary conditions Writing SU2 data transfer files Writing SU2 Motion File - aeroelasticIterative_motion.dat Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.4.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.4.0 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2022, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 10 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 7.74597 m. Reference origin for moment evaluation is (0.322749, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 80092 grid points. 446543 volume elements. 2 surface markers. 17936 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 446543 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 3.71806e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 431.689. Mean K: 20.6394. Standard deviation K: 49.3924. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 50.4346| 86.8674| | CV Face Area Aspect Ratio| 1.06131| 147.499| | CV Sub-Volume Ratio| 1| 867.588| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 80092| 1/1.00| 10| | 1| 13198| 1/6.07| 8.22364| | 2| 2029| 1/6.5| 6.60815| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.53011 m^2, y-plane = 0.868549 m^2, z-plane = 9.83638 m^2. Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m. Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.5258e+00| -1.760106| 0.458269| 0.059417| 3.709000| -0.551171| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.3290e+00| -1.523402| 0.778247| 0.598774| 3.943910| -0.298028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.2913e+00| -1.564337| 0.934465| 0.804042| 3.898737| 1.781382| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.3464e+00| -1.687300| 0.972375| 0.830375| 3.778686| -8.390894| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.2680e+00| -1.556046| 0.864096| 0.698404| 3.908170| -5.334485| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.55605| < -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 = 8970 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.247884e+09, tgt = 6.247884e+09, diff = 2.561357e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.100645e+09, tgt = 6.100645e+09, diff = 7.676172e-01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.122462e+07, tgt = 6.122462e+07, diff = 0.000000e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.121368e+07, tgt = 6.121368e+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 (7.4.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.4.0 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Mesh Deformation Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2022, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- ----------------- Physical Case Definition ( Zone 0 ) ------------------- Input mesh file name: ../aflr3/aflr3_0.su2 ---------------- Grid deformation parameters ( Zone 0 ) ---------------- Grid deformation using a linear elasticity method. -------------------- Output Information ( Zone 0 ) ---------------------- Output mesh file name: aeroelasticIterative.su2. Cell stiffness scaled by distance to nearest solid surface. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ Three dimensional problem. 80092 grid points. 446543 volume elements. 2 surface markers. 17936 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 446543 tetrahedra. ----------------------- Preprocessing computations ---------------------- Setting local point connectivity. Checking the numerical grid orientation of the interior elements. All volume elements are correctly orientend. All surface elements are correctly orientend. Identify edges and vertices. Setting the bound control volume structure. Volume of the computational grid: 3.71806e+06. Info: Ignoring the following volume output fields/groups: SOLUTION Volume output fields: COORDINATES Info: Ignoring the following screen output fields: RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME Info: Ignoring the following history output groups: RMS_RES, AERO_COEFF History output group(s): ITER, TIME_DOMAIN, WALL_TIME Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive. Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. --------------------- Surface grid deformation (ZONE 0) ----------------- Performing the deformation of the surface grid. Updating the surface coordinates from the input file. ------------------- Volumetric grid deformation (ZONE 0) ---------------- Performing the deformation of the volumetric grid. WARNING: Convexity is not checked for 3D elements (issue #1171). ----------------------- Write deformed grid files ----------------------- |SU2 mesh |aeroelasticIterative.su2 | |CSV file |surface_deformed.csv | |Tecplot binary |volume_deformed.szplt | |Tecplot binary surface |surface_deformed.szplt | Adding any FFD information to the SU2 file. ------------------------- Solver Postprocessing ------------------------- Deleted CGeometry container. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted COutput class. Completed in 24.776556 seconds on 1 core. ------------------------- Exit Success (SU2_DEF) ------------------------ ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 7.4.0 "Blackbird" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2022, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.294118. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 10 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 7.74597 m. Reference origin for moment evaluation is (0.322749, 0, 0). Surface(s) where the force coefficients are evaluated: BC_1. Surface(s) plotted in the output file: BC_1. Surface(s) affected by the design variables: BC_1. Input mesh file name: ../aflr3/aflr3_0.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 5. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat. Surface file name: surface_flow_aeroelasticIterative. Volume file name: flow_aeroelasticIterative. Restart file name: restart_flow_aeroelasticIterative.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_1| +-----------------------------------------------------------------------+ | Far-field| BC_2| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Three dimensional problem. 80092 grid points. 446543 volume elements. 2 surface markers. 17936 boundary elements in index 0 (Marker = BC_1). 636 boundary elements in index 1 (Marker = BC_2). 446543 tetrahedra. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. All volume elements are correctly orientend. All surface elements are correctly orientend. Identifying edges and vertices. Setting the control volume structure. Volume of the computational grid: 3.71806e+06. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 431.689. Mean K: 20.6394. Standard deviation K: 49.3924. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 50.4346| 86.8674| | CV Face Area Aspect Ratio| 1.06131| 147.499| | CV Sub-Volume Ratio| 1| 867.588| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 80092| 1/1.00| 10| | 1| 13198| 1/6.07| 8.22364| | 2| 2029| 1/6.5| 6.60815| +-------------------------------------------+ Finding max control volume width. Semi-span length = 3.87298 m. Wetted area = 20.5583 m^2. Area projection in the x-plane = 1.53011 m^2, y-plane = 0.868549 m^2, z-plane = 9.83638 m^2. Max. coordinate in the x-direction = 2.37421 m, y-direction = 3.87298 m, z-direction = 0.399868 m. Min. coordinate in the x-direction = 0 m, y-direction = -3.87298 m, z-direction = -0.0329598 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_1 is NOT a single plane. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 211798| 1| m^2/s^2| 211798| | Velocity-X| 100.087| 1| m/s| 100.087| | Velocity-Y| 0| 1| m/s| 0| | Velocity-Z| 0| 1| m/s| 0| | Velocity Magnitude| 100.087| 1| m/s| 100.087| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.294118| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.7838e+00| -1.760106| 0.458269| 0.059417| 3.709000| -0.551171| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.6522e+00| -1.523402| 0.778247| 0.598774| 3.943910| -0.298028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6249e+00| -1.564337| 0.934465| 0.804042| 3.898737| 1.781382| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.6438e+00| -1.687300| 0.972375| 0.830375| 3.778686| -8.390894| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.6059e+00| -1.556046| 0.864096| 0.698404| 3.908170| -5.334485| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 5) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.55605| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_aeroelasticIterative.dat| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |CSV file |surface_flow_aeroelasticIterative.csv| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary |flow_aeroelasticIterative.szplt | Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). |Tecplot binary surface |surface_flow_aeroelasticIterative.szplt| Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat). +-----------------------------------------------------------------------+ ------------------------- Solver Postprocessing ------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ ==> Running SU2 post-analysis... ==> Running ASTROS pre-analysis... Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure' Rank 0: src = 6.247884e+09, tgt = 6.247884e+09, diff = 2.561357e+02 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure' Rank 0: src = 6.100645e+09, tgt = 6.100645e+09, diff = 7.676172e-01 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure' Rank 0: src = 6.122462e+07, tgt = 6.122462e+07, diff = 0.000000e+00 Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv Number of variables = 13 Number of data points = 8970 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure' Rank 0: src = 6.121368e+07, tgt = 6.121368e+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 4m14.861s user 3m30.272s sys 0m7.743s + 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/7.4/CAPS/training/DARWINM1') [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/7.4/CAPS/training/DARWINM1') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/training/DARWINM1') [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/7.4/CAPS/training/DARWINM1') [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/7.4/CAPS/training/DARWINM1') [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/7.4/CAPS/training/DARWINM1') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.4,CAPS/training,DARWINM1,viggen) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/training,ESP_ARCH=DARWINM1,buildnode=viggen #177' 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=7.4,ESPTEST=CAPS/training,ESP_ARCH=DARWINM1,buildnode=viggen #178'. [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