Hysteresis behavior of shock train driven by continuous incoming Mach number variation in an isolator with background waves

Author:

Wang Ziao,Xin Xuanan,Guo Jifeng,Yue Lianjie,Kong Chen,Huang Renzhe,Chang Juntao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Mathematical Physics

Reference50 articles.

1. Pseudo-shock waves and their interactions in high-speed intakes;Gnani;Prog. Aerosp. Sci.,2016

2. Research progress on strut-equipped supersonic combustors for scramjet application;Chang;Prog. Aerosp. Sci.,2018

3. Oscillation of the shock train in an isolator with incident shocks;Li;Phys. Fluids,2018

4. Separation induced low-frequency unsteadiness in a supersonic combustor with single-side expansion;Chen;Phys. Fluids,2019

5. Isolator characteristics under steady and oscillatory back pressures;Saravanan;Phys. Fluids,2020

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