| 6054
|
COMP MAX EFFECTIVE STRAIN
|
2-Dimensional composite laminate element maximum effective strain (von Mises). Controlled by
STRESS or
STRAIN Case Control commands.
|
| 6055
|
COMP MAX EQUIVALENT STRESS
|
2-Dimensional composite laminate element maximum equivalent stress (von Mises). Controlled by STRESS or STRAIN Case Control commands.
|
| 6060
|
COMP MAX STABILITY FAILURE INDEX
|
2-Dimensional composite sandwich element maximum face sheet stability index. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the
PCOMP entry.
|
| 6061
|
COMP MIN STABILITY FAILURE INDEX
|
2-Dimensional composite sandwich element minimum face sheet stability index. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 6064
|
COMP MIN STABILITY ALLOWABLE
|
2-Dimensional composite sandwich element minimum stability allowable. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 6065
|
COMP MIN STABILITY ALLOWABLE PLY
|
2-Dimensional composite sandwich element minimum stability allowable ply. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 6066
|
COMP STABILITY CORE PLY
|
2-Dimensional composite sandwich element core ply selected by solver. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 6079
|
COMP MAX NORMAL-1 STRESS
|
2-Dimensional composite laminate element maximum ply normal stress in material 1-direction (of all plies). Controlled by
STRESS Case Control command.
|
| 6080
|
COMP MAX NORMAL-2 STRESS
|
2-Dimensional composite laminate element maximum ply normal stress in material 2-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6081
|
COMP MAX SHEAR-12 STRESS
|
2-Dimensional composite laminate element maximum ply shear stress in material 12-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6082
|
COMP MAX SHEAR-XZ STRESS
|
2-Dimensional composite laminate element maximum interlaminar shear stress in material xz-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6083
|
COMP MAX SHEAR-YZ STRESS
|
2-Dimensional composite laminate element maximum interlaminar shear stress in material yz-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6084
|
COMP MIN NORMAL-1 STRESS
|
2-Dimensional composite laminate element minimum ply normal stress in material 1-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6085
|
COMP MIN NORMAL-2 STRESS
|
2-Dimensional composite laminate element minimum ply normal stress in material 2-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6086
|
COMP MIN SHEAR-12 STRESS
|
2-Dimensional composite laminate element minimum ply shear stress in material 12-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6087
|
COMP MIN SHEAR-XZ STRESS
|
2-Dimensional composite laminate element minimum interlaminar shear stress in material xz-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6088
|
COMP MIN SHEAR-YZ STRESS
|
2-Dimensional composite laminate element minimum interlaminar shear stress in material yz-direction (of all plies). Controlled by STRESS Case Control command.
|
| 6089
|
COMP MAX NORMAL-1 STRAIN
|
2-Dimensional composite laminate element maximum ply normal strain in material 1-direction (of all plies). Controlled by
STRAIN Case Control command.
|
| 6090
|
COMP MAX NORMAL-2 STRAIN
|
2-Dimensional composite laminate element maximum ply normal strain in material 2-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6091
|
COMP MAX SHEAR-12 STRAIN
|
2-Dimensional composite laminate element maximum ply shear strain in material 12-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6092
|
COMP MAX SHEAR-XZ STRAIN
|
2-Dimensional composite laminate element maximum interlaminar shear strain in material xz-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6093
|
COMP MAX SHEAR-YZ STRAIN
|
2-Dimensional composite laminate element maximum interlaminar shear strain in material yz-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6094
|
COMP MIN NORMAL-1 STRAIN
|
2-Dimensional composite laminate element minimum ply normal strain in material 1-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6095
|
COMP MIN NORMAL-2 STRAIN
|
2-Dimensional composite laminate element minimum ply normal strain in material 2-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6096
|
COMP MIN SHEAR-12 STRAIN
|
2-Dimensional composite laminate element minimum ply shear strain in material 12-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6097
|
COMP MIN SHEAR-XZ STRAIN
|
2-Dimensional composite laminate element minimum interlaminar shear strain in material xz-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6098
|
COMP MIN SHEAR-YZ STRAIN
|
2-Dimensional composite laminate element minimum interlaminar shear strain in material yz-direction (of all plies). Controlled by STRAIN Case Control command.
|
| 6099
|
COMP MAX PLY FAILURE INDEX
|
2-Dimensional composite laminate element maximum ply failure index (of all plies). Controlled by
STRESS or
STRAIN Case Control commands.
|
| 6099
|
COMP MAX PLY STRENGTH RATIO
|
2-Dimensional composite laminate element maximum ply strength ratio (of all plies). Controlled by STRESS or STRAIN Case Control commands and PARAM,
STRENGTHRATIO.
|
| 6100
|
COMP MAX BOND FAILURE INDEX
|
2-Dimensional composite laminate element maximum bond failure index (of all plies). Controlled by STRESS or STRAIN Case Control commands.
|
| 6100
|
COMP MAX BOND STRENGTH RATIO
|
2-Dimensional composite laminate element maximum bond strength ratio (of all plies). Controlled by STRESS or STRAIN Case Control commands and PARAM, STRENGTHRATIO.
|
| 6101
|
COMP MIN PLY FAILURE INDEX
|
2-Dimensional composite laminate element minimum ply failure index (of all plies). Controlled by STRESS or STRAIN Case Control commands.
|
| 6101
|
COMP MIN PLY STRENGTH RATIO
|
2-Dimensional composite laminate element minimum ply strength ratio (of all plies). Controlled by STRESS or STRAIN Case Control commands and PARAM, STRENGTHRATIO.
|
| 6102
|
COMP MIN BOND FAILURE INDEX
|
2-Dimensional composite laminate element minimum bond failure index (of all plies). Controlled by STRESS or STRAIN Case Control commands.
|
| 6102
|
COMP MIN BOND STRENGTH RATIO
|
2-Dimensional composite laminate element minimum bond strength ratio (of all plies). Controlled by STRESS or STRAIN Case Control commands and PARAM, STRENGTHRATIO.
|
| 6103
|
COMP MAX FAILURE INDEX
|
2-Dimensional composite laminate element maximum failure index (both ply and bond of all plies). Controlled by STRESS or STRAIN Case Control commands.
|
| 6103
|
COMP MIN STRENGTH RATIO
|
2-Dimensional composite laminate element minimum strength ratio (both ply and bond of all plies). Controlled by STRESS or STRAIN Case Control commands and PARAM, STRENGTHRATIO.
|
| 6104
|
COMP MAX FAILURE INDEX PLY
|
2-Dimensional composite laminate element maximum failure index ply (both ply and bond of all plies). Controlled by STRESS or STRAIN Case Control commands.
|
| 6104
|
COMP MIN STRENGTH RATIO PLY
|
2-Dimensional composite laminate element maximum failure index ply (both ply and bond of all plies). Controlled by STRESS or STRAIN Case Control commands and PARAM, STRENGTHRATIO.
|
| 6109
|
COMP MAX PRINCIPAL STRESS
|
2-Dimensional composite laminate element maximum ply principal stress (of all plies). Controlled by
STRESS Case Control command.
|
| 6110
|
COMP MIN PRINCIPAL STRESS
|
2-Dimensional composite laminate element minimum ply principal stress (of all plies). Controlled by STRESS Case Control command.
|
| 6111
|
COMP MAX MAX SHEAR STRESS
|
2-Dimensional composite laminate element maximum maximum shear stress (of all plies). Controlled by STRESS Case Control command.
|
| 6112
|
COMP MAX VON MISES STRESS
|
2-Dimensional composite laminate element maximum von Mises stress (of all plies). Controlled by STRESS Case Control command.
|
| 6113
|
COMP MAX PRINCIPAL STRAIN
|
2-Dimensional composite laminate element maximum ply principal strain (of all plies). Controlled by
STRAIN Case Control command.
|
| 6114
|
COMP MIN PRINCIPAL STRAIN
|
2-Dimensional composite laminate element minimum ply principal strain (of all plies). Controlled by STRAIN Case Control command.
|
| 6115
|
COMP MAX MAX SHEAR STRAIN
|
2-Dimensional composite laminate element maximum maximum shear strain (of all plies). Controlled by STRAIN Case Control command.
|
| 6116
|
COMP MAX VON MISES STRAIN
|
2-Dimensional composite laminate element maximum von Mises strain (of all plies). Controlled by STRAIN Case Control command.
|
| 6117
|
COMP STATUS
|
2-Dimensional composite laminate element ply failure status in percent of total plies failed. Controlled by
STRESS or
STRAIN Case Control commands and PARAM,
NLCOMPPLYFAIL.
|
| 7206
|
COMP MEMBRANE FORCE-FX
|
2-Dimensional composite laminate element inplane normal force per unit length in
SURFACE x-direction. Controlled by
FORCE Case Control command.
|
| 7207
|
COMP MEMBRANE FORCE-FY
|
2-Dimensional composite laminate element inplane normal force per unit length in SURFACE y-direction. Controlled by FORCE Case Control command.
|
| 7208
|
COMP MEMBRANE FORCE-FXY
|
2-Dimensional composite laminate element inplane shear force per unit length in SURFACE xy-direction (tensor x-face, y-direction). Controlled by FORCE Case Control command.
|
| 7211
|
COMP BENDING MOMENT-MX
|
2-Dimensional composite laminate element bending moment per unit length in SURFACE y-direction. Controlled by FORCE Case Control command.
|
| 7212
|
COMP BENDING MOMENT-MY
|
2-Dimensional composite laminate element bending moment per unit length in SURFACE x-direction. Controlled by FORCE Case Control command.
|
| 7213
|
COMP BENDING MOMENT-MXY
|
2-Dimensional composite laminate element twisting moment per unit length in SURFACE xy-direction (tensor x-face, y-direction). Controlled by FORCE Case Control command.
|
| 7214
|
COMP TRANSVERSE SHEAR FORCE-QX
|
2-Dimensional composite laminate element transverse shear force per unit length in SURFACE xz-direction. Controlled by FORCE Case Control command.
|
| 7215
|
COMP TRANSVERSE SHEAR FORCE-QY
|
2-Dimensional composite laminate element transverse shear force per unit length in SURFACE yz-direction. Controlled by FORCE Case Control command.
|
| 1000020 + 200(ply - 1)
|
COMP PLY NORMAL-1 STRESS
|
2-Dimensional composite laminate element ply normal stress in ply 1-direction (longitudinal). Controlled by
STRESS Case Control command.
|
| 1000021 + 200(ply - 1)
|
COMP PLY NORMAL-2 STRESS
|
2-Dimensional composite laminate element ply normal stress in ply 2-direction (lateral). Controlled by STRESS Case Control command.
|
| 1000023 + 200(ply - 1)
|
COMP PLY SHEAR-12 STRESS
|
2-Dimensional composite laminate element ply normal stress in ply 12-direction. Controlled by STRESS Case Control command.
|
| 1000024 + 200(ply - 1)
|
COMP PLY SHEAR-XZ STRESS
|
2-Dimensional composite laminate element interlaminar shear stress in material xz-direction. Controlled by STRESS Case Control command.
|
| 1000025 + 200(ply - 1)
|
COMP PLY SHEAR-YZ STRESS
|
2-Dimensional composite laminate element interlaminar shear stress in material yz-direction. Controlled by STRESS Case Control command.
|
| 1000026 + 200(ply - 1)
|
COMP PLY MAX PRINCIPAL STRESS
|
2-Dimensional composite laminate element ply maximum principal stress. Controlled by STRESS Case Control command.
|
| 1000027 + 200(ply - 1)
|
COMP PLY MIN PRINCIPAL STRESS
|
2-Dimensional composite laminate element ply minimum principal stress. Controlled by STRESS Case Control command.
|
| 1000031 + 200(ply - 1)
|
COMP PLY MAX SHEAR STRESS
|
2-Dimensional composite laminate element ply maximum shear stress. Controlled by STRESS Case Control command.
|
| 1000032 + 200(ply - 1)
|
COMP PLY EQUIVALENT STRESS
|
2-Dimensional composite laminate element equivalent stress (von Mises). Controlled by
STRESS or
STRAIN Case Control commands.
|
| 1000033 + 200(ply - 1)
|
COMP PLY VON MISES STRESS
|
2-Dimensional composite laminate element von Mises stress. Controlled by STRESS Case Control command.
|
| 1000090 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX
|
2-Dimensional composite laminate element ply ply failure index. Controlled by STRESS or STRAIN Case Control commands.
|
| 1000090 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO
|
2-Dimensional composite laminate element ply ply strength ratio. Controlled by STRESS or STRAIN Case Control commands and PARAM,
STRENGTHRATIO.
|
| 1000091 + 200(ply - 1)
|
COMP PLY BOND FAILURE INDEX
|
2-Dimensional composite laminate element ply bond failure index. Controlled by STRESS or STRAIN Case Control commands.
|
| 1000091 + 200(ply - 1)
|
COMP PLY BOND STRENGTH RATIO
|
2-Dimensional composite laminate element ply bond strength ratio. Controlled by STRESS or STRAIN Case Control commands.
|
| 1000092 + 200(ply - 1)
|
COMP PLY STABILITY INDEX
|
2-Dimensional composite sandwich element face sheet stability index. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000093 + 200(ply - 1)
|
COMP PLY STABILITY ALLOWABLE
|
2-Dimensional composite sandwich element stability allowable (minimum of the wrinkling, dimpling, and crimping allowables). Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000094 + 200(ply - 1)
|
COMP PLY STABILITY ALLOWABLE FAILURE MODE
|
2-Dimensional composite sandwich element stability allowable failure mode (1=wrinkling, 2=dimpling, 3=crimping). Controlled by
STRESS or
STRAIN Case Control commands and the LAM field on the
PCOMP entry.
|
| 1000095 + 200(ply - 1)
|
COMP PLY STABILITY INDEX WRINKLING
|
2-Dimensional composite sandwich element face sheet wrinkling stability index. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000096 + 200(ply - 1)
|
COMP PLY STABILITY INDEX DIMPLING
|
2-Dimensional composite sandwich element face sheet dimpling stability index. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000097 + 200(ply - 1)
|
COMP PLY STABILITY INDEX CRIMPING
|
2-Dimensional composite sandwich element face sheet crimping stability index. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000098 + 200(ply - 1)
|
COMP PLY STABILITY ALLOWABLE WRINKLING
|
2-Dimensional composite sandwich element wrinkling stability allowable. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000099 + 200(ply - 1)
|
COMP PLY STABILITY ALLOWABLE DIMPLING
|
2-Dimensional composite sandwich element dimpling stability allowable. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000000 + 200(ply - 1)
|
COMP PLY STABILITY ALLOWABLE CRIMPING
|
2-Dimensional composite sandwich element crimping stability allowable. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.
|
| 1000101 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX MATRIX-TENSION
|
2-Dimensional composite laminate element ply matrix-tension failure index (LaRC02 or Puck failure theories). Controlled by
STRESS or
STRAIN Case Control commands and the FT field on the
PCOMP entry.
|
| 1000101 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX MATRIX-1
|
2-Dimensional composite laminate element ply matrix failure index (MCT failure theory). Fill-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000101 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO MATRIX-TENSION
|
2-Dimensional composite laminate element ply matrix-tension failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000101 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO MATRIX-1
|
2-Dimensional composite laminate element ply matrix strength ratio (MCT failure theory). Fill-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000102 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX MATRIX-COMPRESSION
|
2-Dimensional composite laminate element ply matrix-compression failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000102 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX MATRIX-2
|
2-Dimensional composite laminate element ply matrix failure index (MCT failure theory). Warp-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000102 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO MATRIX-COMPRESSION
|
2-Dimensional composite laminate element ply matrix-compression failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000102 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO MATRIX-2
|
2-Dimensional composite laminate element ply matrix strength ratio (MCT failure theory). Warp-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000103 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX FIBER-TENSION
|
2-Dimensional composite laminate element ply fiber-tension failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000103 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX FIBER-1
|
2-Dimensional composite laminate element ply fiber failure index (MCT failure theory). Fill-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000103 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO FIBER-TENSION
|
2-Dimensional composite laminate element ply fiber-tension failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000103 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO FIBER-1
|
2-Dimensional composite laminate element ply fiber strength ratio (MCT failure theory). Fill-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000104 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX FIBER-COMPRESSION
|
2-Dimensional composite laminate element ply fiber-compression failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000104 + 200(ply - 1)
|
COMP PLY PLY FAILURE INDEX FIBER-2
|
2-Dimensional composite laminate element ply fiber failure index (MCT failure theory). Warp-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000104 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO FIBER-COMPRESSION
|
2-Dimensional composite laminate element ply fiber-compression failure index (LaRC02 or Puck failure theories). Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000104 + 200(ply - 1)
|
COMP PLY PLY STRENGTH RATIO FIBER-2
|
2-Dimensional composite laminate element ply fiber failure index (MCT failure theory). Warp-direction for plain weave fabrics. Controlled by STRESS or STRAIN Case Control commands and the FT field on the PCOMP entry.
|
| 1000105 + 200(ply - 1)
|
COMP PLY FAILURE THEORY
|
2-Dimensional composite laminate failure theory code [1=Hill, 2=Hoffman, 3=Tsai-Wu, 4=Max Strain (MSC), 5=Max Strain (Autodesk), 6=Max Stress, 7=LaRC02, 8=Puck, 9=MCT, 0=None]. Controlled by the FT field on the
PCOMP Bulk Data entry.
|
| 1000106 + 200(ply - 1)
|
COMP PLY FRACTURE ANGLE
|
2-Dimensional composite laminate fracture plane angle (LaRC02 and Puck failure theories only). Controlled by STRESS or STRAIN Case Control commands.
|
| 1000107 + 200(ply - 1)
|
COMP PLY STRENGTH RATIO ERROR
|
2-Dimensional composite laminate element strength ratio error. Controlled by STRESS or STRAIN Case Control commands.
|
| 1000108 + 200(ply - 1)
|
COMP PLY STATUS
|
2-Dimensional composite laminate element ply failure status (1=ply has failed, 0=ply has not failed). Controlled by
STRESS or
STRAIN Case Control commands and PARAM,
NLCOMPPLYFAIL.
|
| 1000109 + 200(ply - 1)
|
COMP PLY EFFECTIVE STRAIN
|
2-Dimensional composite laminate element effective strain (von Mises). Controlled by STRESS or STRAIN Case Control commands.
|