Expansion of the scramjet ground test envelope of the Hypulse facility
Author:
Affiliation:
1. GASL, Inc., Ronkonkoma, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-4506
Reference12 articles.
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4. Simulation of High Mach Number Scramjet Flow Conditions using the X2 Expansion Tube;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24
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