| Vector Id | Label | Description |
|---|---|---|
| 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. |
|
1000126 + 200(ply - 1) |
COMP PLY PFA DAMAGE STATE | 2-Dimensional composite laminate element PFA damage state for Helius PFA composite material. |