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Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element minimum interlaminar shear stress in material xz-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element minimum ply shear stress in material 12-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element minimum ply normal stress in material 2-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element minimum ply normal stress in material 1-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element maximum interlaminar shear stress in material yz-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element maximum interlaminar shear stress in material xz-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element maximum ply shear stress in material 12-direction (of all plies). Controlled by STRESS Case Control command.Ģ-Dimensional composite laminate element maximum ply normal stress in material 2-direction (of all plies). Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.Ģ-Dimensional composite laminate element maximum ply normal stress in material 1-direction (of all plies). Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.Ģ-Dimensional composite sandwich element core ply selected by solver.
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![element 3d 2.2 auto-normals element 3d 2.2 auto-normals](https://www.videocopilot.net/assets/public/ckfinder/userfiles/images/texturing_and_materials/UV-differences-thumb(1).jpg)
Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.Ģ-Dimensional composite sandwich element minimum stability allowable ply. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.Ģ-Dimensional composite sandwich element minimum stability allowable. Controlled by STRESS or STRAIN Case Control commands and the LAM field on the PCOMP entry.Ģ-Dimensional composite sandwich element minimum face sheet stability index. Controlled by STRESS or STRAIN Case Control commands.Ģ-Dimensional composite sandwich element maximum face sheet stability index. Controlled by STRESS or STRAIN Case Control commands.Ģ-Dimensional composite laminate element maximum equivalent stress (von Mises). 2-Dimensional composite laminate element maximum effective strain (von Mises).