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The optimal positioning of leading-edge stringers for the cruise condition was determined in this study through the optimization of equivalent stress in fluid-structure coupling. The Watt-I six-bar mechanism in the skeletal structure of leading-edge droop was proposed.
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This page is a summary of: Design and Aerodynamic Analysis of Leading Edge for Morphing Wing, Journal of Aircraft, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c038158.
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