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For the first time in the literature it is shown that 2 widely used approaches for the analysis of composites (Hellinger-Reissner and Reissner's mixed Variational Theorem) provide under certain conditions identical results and also have non-physical oscillations of the values for the displacements and stresses. Remedies are proposed and investigated.

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This page is a summary of: Modeling Challenges and Limitation Principles of Reissner’s Mixed Approaches to Laminates, AIAA Journal, January 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063821.
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