Shock wave structures in the wake of sonic transverse jet into a supersonic crossflow
Author:
Funder
National Natural Science Foundation of China
National University of Defense Technology
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference27 articles.
1. Effects of oblique and transverse injection on the characteristics of jet in supersonic crossflow;Zhang;Acta Astronaut.,2015
2. Large Eddy Simulation of the fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity;Cai;Acta Astronaut.,2016
3. Transverse jets and their control;Karagozian;Prog. Energy Combust. Sci.,2010
4. The interaction of jets with crossflow;Mahesh;Annu. Rev. Fluid Mech.,2013
5. Shock/boundary-layer interaction effects on transverse jets in crossflow over a flat plate;Dickmann;J. Spacecraft Rockets,2015
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