Detail Composite Analysis With SAMCEF
Composite modeling in SAMCEF is not limited to a specific kind of analysis. Linear static, buckling and modal analyses, as well as transient and harmonic responses, thermo-mechanical, non-linear static and dynamic analyses ( for post-buckling and collapse simulations) are indeed supported. Laminates including layered and sandwich materials can be assigned to models made of membranes, shells and volume elements. Specific axisymmetric and multi-harmonic solutions are also available for modeling filament wound structures. SAMCEF offers a ply by ply result recovery, for the classical failure criteria ( maximum stress, Tsai-Hill, Tsai-Wu, Hashin, Puck) . Advanced non-linear material effects can also be modeled, such as the progressive delamination at the interface of the plies. The progressive damage inside the plies leading to the fiber breaking and the matrix cracking can also be simulated. A specific material law coupling inter and intra-laminar damages is also available.
Features
SAMCEF allows you to study your composite structure with respect to stiffness, strength, geometric non-linear effects such as post-buckling, and progressive material degradation.
Benefits
The Composite Analysis capabilities available in SAMCEF allow you to:
• Model layered materials for membrane, shell, volume and axisymmetric structures
• Accurately predict the stiffness and strength responses of the composite structure
• Accurately simulate the geometric non-linear behavior of the composite structure
• Accurately simulate the progressive degradation of your layered composite structure, including delamination and damage inside the ply
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0815 614 1954, 0811 891 101, 0817921 7081
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