Design, calibration and analysis of a tunnel mode of operation for the HYPULSE facility

Author:

Bakos R.1,Calleja J.1,Erdos J.1,Auslender A.2,Sussman M.3,Wilson G.3

Affiliation:

1. General Applied Science Labs., Inc., Ronkonkoma, NY

2. Lockheed Engineering & Sciences Co., Hampton, VA

3. Thermosciences Inst., Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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2. Expansion Tubes in Australia;Experimental Methods of Shock Wave Research;2015-11-01

3. Production of High-Mach-Number Scramjet Flow Conditions in an Expansion Tube;AIAA Journal;2014-01

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

5. Nozzle development for an expansion tunnel;Shock Waves;2005

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