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机译:Multi-objective aerodynamic optimization of an axisymmetric variable-geometry inlet with a Mach 5 design point
Research Institute of Aero-Engine, Beihang University, Beijing, 100191 China;
School of Energy and Power Engineering, Beihang University, Beijing, 100191, China;
Beijing Institute of Mechanical and Electrical Engineering, Beijing, 100074, China;
Axisymmetric variable-geometry inlet; Hypersonic speed; Total pressure recovery; Multi-objective optimization; Wind tunnel experiment; Computational fluid dynamics;