Laminate Composites > Solution and post processing > Laminate results
Shell stress resultant notations
| Laminate Composites | Nastran | Abaqus | ANSYS | Pre/Post Post Processing |
|---|---|---|---|---|
| Nx | Fx | SF1 | N11 | Nxx |
| Ny | Fy | SF2 | N22 | Nyy |
| Nxy | Fxy | SF3 | N12 | Nxy |
| Mx (-Mx wrt Nastran) | Mx | SM1 | M11 | Mxx |
| My (-My wrt Nastran) | My | SM2 | M22 | Myy |
| Mxy (-Mxy wrt Nastran) | Mxy | SM3 | M12 | Mxy |
| Qx | Vx | SF5 | Q13 | Qyz |
| Qy | Vy | SF4 | Q23 | Qxz |
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View laminate physical properties for a selected element in post processing
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Shell stress resultant notations, Simcenter 3D 2021.1 Series
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Source: https://docs.sw.siemens.com/en-US/doc/289054037/PL20200601120302950.advanced/genid_shell_stress_resultant_notations_287_466 · retrieved 2026-07-17