Scramjet testing in the T4 impulse facility-Reference-Cited by-同舟云学术

Scramjet testing in the T4 impulse facility

Published:1998-04-27 Issue: Volume: Page:
ISSN:
Container-title:8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Paull A.¹,Stalker R.¹

Affiliation:

1. Queensland, Univ., Brisbane, Australia

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1533

Reference9 articles.

1. Boyce R.R,Wendt M, Paull A, Chinzei N, Stalker R.J. and Miyajima H. Supersonic combustion - a shock tunnel and vitiation-heated blowdown tunnel comparison, 36th Aerospace Sc., Reno AIAA 98-0941

2. Comparison of Shock-Induced Two- and Three- Dimensional Incipient Turbulent Seperation

3. Mee, D.J.,Daniel,WJ.T andSimmons,J.M.1996, A three component force balance for flows of a millisecondduration,AIAAJ.34(3)pp.590-595

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