Mechanism of shock-train/boundary-layer interaction in spanwise concave isolator channels
Author:
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
State Key Laboratory of High Temperature Gas Dynamics
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference39 articles.
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3. Effect of cavity pressure on shock train behavior and panel aeroelasticity in an isolator;Physics of Fluids;2022-12
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