Scaling of interaction lengths for hypersonic shock wave/turbulent boundary layer interactions
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference34 articles.
1. Shock wave-boundary layer interactions;Babinsky,2011
2. Fifty years of shock-wave/boundary-layer interaction research: What next?;Dolling;AIAA J,2001
3. Separation shock motion in fin, cylinder, and compression ramp-induced turbulent interactions;Dolling;AIAA J,1989
4. Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions;Clemens;Annu Rev Fluid Mech,2014
5. Progress in shock wave/boundary layer interactions;Gaitonde;Prog Aerosp Sci,2015
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