Forced oscillation phenomenon of normal/oblique shock trains in a rectangular duct at Mach 2 and 3

Author:

Yi Wang,Bing Xiong,Xiaoqiang Fan

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl;Wen;Acta Astronaut.,2018

2. Aerodynamic performance analysis of a hypersonic inlet isolator using computation and experiment;Reinartz;J. Propul. Power,2003

3. Large-eddy simulations of a normal shock train in a constant-area isolator;Morgan;AIAA J.,2014

4. Preliminary study of shock train in a curved variable-section diffuser;Tan;J. Propul. Power,2008

5. Structure and Oscillation Phenomena of Pseudo-shock Waves in a Straight Square Duct at Mach 2 and 4;Sugiyama,2008

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