Measured effects of shock waves on supersonic hydrogen-air flames-Reference-Cited by-同舟云学术

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Measured effects of shock waves on supersonic hydrogen-air flames

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
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Author:

Huh Hwanil¹,Driscoll James¹

Affiliation:

1. Michigan, Univ., Ann Arbor

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3035

Reference27 articles.

1. Blowout Stability Limits Of a Hydrogen Jet Flame In a Supersonic, Heated, Coflowinq Air Stream

2. 'Driscoll, J.F., Huh, H., Yoon, Y. and Donbar, J. "Measured Lengths of Supersonic Hydrogen Air Flames,"toappearin Combust.Flame,1996.

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2. Swirl Effects on Free Underexpanded Supersonic Airflow;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

3. Swirl Effects on Shock Structure in Free Under-Expanded Supersonic-Nozzle Airflow;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

4. Numerical Investigation of Oblique Fuel Injection in a Supersonic Combustor;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

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