Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Funder
Fundamental Research Funds for the Central Universities
China Postdoctoral Science Foundation
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Reference18 articles.
1. Possibilities for Improved Supersonic Inlet Performance
2. JohnsonH. J.MontoyaE. J. “Local Flow Measurements at the Inlet Spike Tip of a Mach 3 Supersonic Cruise Airplane,” NASA TN D-6987, May 1973.
3. Numerical and experimental analysis of a hypersonic variable geometry inlet
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