NASA NTRS · 19920050168
An approximate analytical solution for interlaminar stresses in angle-ply laminates
Abstract
An improved approximate analytical solution for interlaminar stresses in finite width, symmetric, angle-ply laminated coupons subjected to axial loading is presented. The solution is based upon statically admissible stress fields which take into consideration local property mismatch effects and global equilibrium requirements. Unknown constants in the admissible stress states are determined through minimization of the complementary energy. Typical results are presented for through-the-thickness and interlaminar stress distributions for angle-ply laminates. It is shown that the results represent an improved approximate analytical solution for interlaminar stresses.
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Rose, Cheryl A., Herakovich, Carl T.. 1991-01-01. An approximate analytical solution for interlaminar stresses in angle-ply laminates. https://ntrs.nasa.gov/citations/19920050168
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