Evolution of supersonic corner vortex in a hypersonic inlet/isolator model
Author:
Affiliation:
1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2. College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Funder
National Natural Science Foundation of China (NSFC)
Program for New Century Excellent Talents in University (NCET)
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4971448
Reference45 articles.
1. Scramjets
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5. Structure of Flow over a Hypersonic Inlet with Side Compression Wedges
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