Experimental study of the effect of nose temperature on the disturbance waves in hypersonic boundary layer of blunted cone
1College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2Key Laboratory of Unsteady Aerodynamics and Flow Control, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
3State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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