2021
DOI: 10.2514/1.j059364
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Skin-Stringer Assembly Using Radial Basis Functions for Curvilinearly Stiffened Panels

Abstract: Recent studies on design optimization of aircraft panels using curvilinear stiffeners reveal that it is possible to improve both the buckling and vibration responses of stiffened structures by varying the stiffener's shape, which change the stiffness as well as the buckling and vibration mode shapes [1][2][3]. Due to the enhanced tailorability of stiffness distribution of stiffened panels, provided by curvilinear stiffeners and curvilinear fiber paths for a plate; Stanford and Jutte [4] studied the aircraft wi… Show more

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Cited by 5 publications
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