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Multidisciplinary Design and Optimization of Variable Camber Wing with Non-Equal Chord
6. Results and Analysis of Multidisciplinary Optimization The multidisciplinary optimization of the non-equal chord morphing wing was integrated using Isight software. The platform consists of two modules: the comprehensive optimization module of aerodynamic and honeycomb structure parameters, and the optimization module of wing structure size. The former mainly completes the establishment of morphing wing geometry and airfoil optimization considering the deformation ability of honeycomb skin.
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