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For each of the problems below, the material is assumed to be carbon (M55 fiber) / epoxy composite with the following properties: E =
For each of the problems below, the material is assumed to be carbon (M55 fiber) / epoxy composite with the following properties: E = 40 Msi E2 = 1.8 Msi V12 = 0.3 G12 = 0.7 Msi X = 230 ksi Xc = -180 ksi Y = 7 ksi Y = -35 ksi S = 10 ksi
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Solutions Step 1 Explanation To compute the midplane strains and curvatures we need to first calcula...
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