Experimental Investigation of the Unstart Process of a Generic Hypersonic Inlet
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050200
Reference19 articles.
1. Experimental Study of the Unstable-Unstarted Condition of a Hypersonic Inlet at Mach 6
2. The Full Flowpath Analysis of a Hypersonic Vehicle
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