Combustion Heat-Release Effects on Supersonic Compressible Turbulent Boundary Layers
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053585
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