Mechanism Study on Local Unstart of Hypersonic Inlet at High Mach Number
Author:
Affiliation:
1. School of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, 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.J053913
Reference38 articles.
1. Airbreathing hypersonic technology vision vehicles and development dreams
2. KantrowitzA.DonaldsonC. “Preliminary Investigation of Supersonic Diffusers,” NACA ACR-L5D20, May 1945.
3. Starting characteristics of supersonic inlets
4. Limiting Contractions for Starting Simple Ramp-Type Scramjet Intakes with Overboard Spillage
5. Prediction of supersonic inlet unstart caused by freestream disturbances
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