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Recent content by Peregrino
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Laminates: setting stiffness tensors in Nastran
Hi, I am reducing the weight of a wingbox which consists of laminate plates. To implement a proper optimization scheme, I need to know how to change laminate stiffness matrices A and D. In Ansys ADPL language, I could type SET,a22b,0.5 #variables init SET,a11b,0.3 ...- Peregrino
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- Forum: Composite engineering
