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For a given areal mass density, the paper optimizes the shell geometry and materials for supporting the maximum pressure applied on the shell top surface. It will provide light weight designs of doubly-curved shells.
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This page is a summary of: Optimum First Failure Loads of One- and Two-Core Doubly Curved Sandwich Shells, AIAA Journal, August 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059238.
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