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Two nonlinear strain-displacements are adopted to model the damaged laminated composite structure in the framework of the higher-order kinematic model. The solution accuracy and the recommended model is verified first time with in-house experimental results.
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This page is a summary of: Numerical Nonlinear Static Analysis of Cutout-Borne Multilayered Structures and Experimental Validation, AIAA Journal, September 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060643.
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