Investigation on conical separation vortex generated by swept shock wave/turbulent boundary layer interaction
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference49 articles.
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4. Progress in shock wave/boundary layer interactions;Gaitonde;Prog. Aerosp. Sci.,2015
5. Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows;Huang;Acta Astronaut.,2020
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