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Fiber-steered nonconventional laminates provide performance increase for cylindrical shells in bending compared to conventional straight fiber ones. Analysis of such shells are performed to evaluate the influence of large circular holes on the stiffness and strength for different hole sizes and locations.

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This page is a summary of: Bending of Composite Cylindrical Shells with Circular Cutouts: Buckling and Failure Analysis, Journal of Aircraft, July 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035246.
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