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机译:Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle
College of Energy and Power Engineering. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
State Key Laboratory of Mechanics and Control of Aeronautics and Astronautics Structures, Nanjing 210016, China ,College of Energy and Power Engineering. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
Sichuan Gas Turbine Establishment, Aero Engine Corporation of China. Chengdu, 610500, China;
Short takeoff and landing (STOL); Bypass dual throat nozzle (BDTN); Transition part; Thrust vectoring;