RDHWT/MARIAH II hypersonic wind tunnel program overview and requirements

Author:

Best J.1,Fetterhoff T.1,Crook R.1,Laster M.2,Jordan J.2

Affiliation:

1. USAF, AEDC, Arnold AFB, TN

2. Sverdrup Technology, Inc., AEDC Group, Arnold AFB, TN

Publisher

American Institute of Aeronautics and Astronautics

Cited by 8 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

1. Time requirements for scramjet performance study with fuel of kerosene;Shock Waves;2005

2. Energy Management for Hypersonic Heat-Sink Nozzles;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15

3. A Hypersonic Ground-Test Facility Using Magnetic Levitation and Electromagnetic Propulsion;Advanced Hypersonic Test Facilities;2002-01-01

4. RDHWT/MARIAH II hypersonic wind tunnel research program update;10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference;2001-04-24

5. Ultra-high pressure driver and nozzle survivability in the RDHWT/MARIAH II hypersonic wind tunnel;21st Aerodynamic Measurement Technology and Ground Testing Conference;2000-06-19

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