Wall heat flux in a supersonic shock wave/turbulent boundary layer interaction
Author:
Affiliation:
1. State Key Laboratory of Aerodynamics, 621000 Mianyang, China
2. LHD, Institute of Mechanics, Chinese Academy of Sciences, 100190 Beijing, China
3. School of Engineering Science, University of Chinese Academy of Sciences, 100049 Beijing, China
Abstract
Funder
National Natural Science Foundation of China
National Key Research and Development Program of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0094070
Reference41 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. Progress in shock wave/boundary layer interactions
3. Correlation of peak heating for reattachment of separated flows.
4. Changes in heat transfer from turbulent boundary layers interacting with shock waves and expansion waves
5. Experimental investigation of axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions
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