Propagation of shock-wave/boundary-layer interaction unsteadiness in attached and separated flows
Author:
Affiliation:
1. Harbin Institute of Technology, Harbin, Heilongjiang 150001, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0023935
Reference51 articles.
1. Progress in shock wave/boundary layer interactions
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3. Unsteadiness in transonic shock-wave/boundary-layer interactions: experimental investigation and global stability analysis
4. Isolator characteristics under steady and oscillatory back pressures
5. Flow field reconstruction and prediction of the supersonic cascade channel based on a symmetry neural network under complex and variable conditions
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