Some numerical investigation results of shock-induced combustion-Reference-Cited by-同舟云学术

Some numerical investigation results of shock-induced combustion

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

Bezgin L.¹,Ganzhelo A.¹,Gouskov O.¹,Kopchenov V.¹

Affiliation:

1. Central Inst. of Aviation Motors, Moscow, Russia

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1513

Reference22 articles.

1. Sislian, J.P., Dudebout, R., Schumacher, J., Oppitz, R. "Inviscid Propulsive Characterstics of Hypersonic Shcramjets," AIAA-96-4535. Gonzalez, D.E. "Computational Study of Inlet Injection for Premixed Shock-Induced Combustion,"AIAA-96-4560.

2. Chinitz, W. "On the Use of Shock-Induced Combustion in Hypersonic Engines," AIAA-96-4536.

3. Humphrey, Joseph W. "Parametric Study of an ODW Scramaccelerator for Hypersonic Test Facilities," AIAA 90-2470.

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