Experimental Investigation of Hysteresis Phenomenon for Scramjet Engine
Author:
Affiliation:
1. Academy of Fundamental and Interdisciplinary Sciences, Harbin Institute of Technology, 150001 Harbin, 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.J052505
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1. High-speed inlet unstart calculations using an implicit solution adaptive mesh algorithm
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5. Time-Frequency Analysis and Detection of Supersonic Inlet Buzz
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