Effects of unsteady oblique shock wave on mixing efficiency of two-dimensional supersonic mixing layer
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference46 articles.
1. Historical survey on enhanced mixing in scramjet engines;Seiner;J. Propul. Power,2001
2. A review on enhanced mixing methods in supersonic mixing layer flows;Tan;Acta Astronaut.,2018
3. Progress toward Shock Enhancement of Supersonic Combustion Processes;Marble,1987
4. On the shock enhancement of confined supersonic mixing flows;Lu;Phys. Fluid. Fluid Dynam.,1991
5. Numerical study of mixing enhancement by shock waves in model scramjet engine;Kim;AIAA J.,2003
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