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High-Fidelity Aeroelastic Computations of a Flapping Wing with Spanwise Flexibility
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
A high-order (up to 6th order) Navier-Stokes solver is coupled with a structural solver that decomposes the equations of three-dimensional elasticity into cross-sectional, smalldeformation and spanwise, large-deformation analyses for slender wings. The resulting high-fidelity aeroelastic solver is applied to the investigation of rigid, moderately flexible and highly flexible rectangular wings undergoing a pure plunging motion. Comparisons of the computed results with available experimentaldoi:10.2514/6.2011-570 fatcat:vpoxnxmvpjcfdgj6uptwlbbmva