Finite element modeling method for variable stiffness composite laminate
A laminated board and variable stiffness technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems that affect research progress, trouble, errors, etc.
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[0023] This embodiment is a finite element modeling method of a variable stiffness composite material laminate.
[0024] refer to figure 1 , figure 2 , the finite element modeling method of variable stiffness composite laminates in this embodiment, based on the above-mentioned operation steps of variable stiffness laminates, the following gives the layup as [±]s, and uses the translation method to realize the curve laying Layers of variable stiffness laminates are described in detail for specific examples.
[0025] The first step is to establish a complete four-layer laminate model in Patran according to the general steps. The lay-up angles of the four single layers are given arbitrarily and submitted for analysis to generate a model file. The fiber angle of the curved ply is , that is, the middle fiber angle of a single layer is 30°, the edge fiber angle is 0°, and the fiber angle is symmetrical about the midpoint. For the convenience of calculation, a local coordinate sys...
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