Unsteady Behaviors of a Hypersonic Inlet Caused by Throttling in Shock Tunnel
Author:
Affiliation:
1. Modern Mechanics Department, University of Science and Technology of China, 230027 Hefei, 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.J052384
Reference16 articles.
1. Starting characteristics of supersonic inlets
2. Hypersonic Airbreathing Propulsion
3. ScottD. H. “Wind-Tunnel Blockage and Actuation Systems Test of a Two-Dimensional Scramjet Inlet Unstart Model at Mach 6,” NASA TM-109152, 1994.
4. Unsteady pressure behavior in a ramjet/scramjet inlet
5. Experimental Study of the Unstable-Unstarted Condition of a Hypersonic Inlet at Mach 6
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