Abstract:This paper proposes an efficient low-speed airfoil selection and design optimization process using multifidelity analysis for a long endurance Unmanned Aerial Vehicle (UAV) flying wing. The developed process includes the low-speed airfoil database construction, airfoil selection and design optimization steps based on the given design requirements. The multi-fidelity analysis solvers including the panel method and computational fluid dynamics (CFD) are presented to analyze the low speed airfoil aerodynamic char… Show more
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