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This paper investigates the use of a special class of composites materials, known as sandwich composites, for the design of commercial aircraft wings. The research is directed towards developing lighter and green future generation of aircraft.
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This page is a summary of: Lamination-Parameter-Based Mass Minimization of the Common Research Model Wing Using Sandwich Composites, Journal of Aircraft, July 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037863.
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