Dynamic flow evolution characteristics and hysteresis mechanisms in translational adjustment of cowlOA
Dynamic flow evolution characteristics and hysteresis mechanisms in translational adjustment of cowl
Hao ZHANG;Yue ZHANG;Hang YU;Huijun TAN;Hongchao XUE;Liang CHEN;Xin LI
Key Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,ChinaKey Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,ChinaKey Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,ChinaKey Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,ChinaKey Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,ChinaKey Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,ChinaDepartment of Aeronautical and Aviation Engineering,The Hong Kong Polytechnic University,999077,Hong Kong,China
Flow oscillationHysteresisUnsteady flowsVariable-geometry inlet
Flow oscillationHysteresisUnsteady flowsVariable-geometry inlet
《中国航空学报（英文版）》 2026 (9)
142-160,19
This work was funded by the National Natural Science Foun-dation of China(Nos.12025202 and 12172175),the Fund of National Key Laboratory of Aerospace Liquid Propulsion,China(No.2024JJ015010).
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