Combustion characteristics of an inlet/supersonic combustor model-Reference-Cited by-同舟云学术

Combustion characteristics of an inlet/supersonic combustor model

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Gamba Mirko¹,Miller Victor¹,Mungal Godfrey²,Hanson Ronald¹

Affiliation:

1. Stanford University

2. Santa Clara University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-612

Reference19 articles.

1. Comparison of NO and OH planar fluorescence temperature measurements in scramjet model flowfield

2. Hypersonic combustion and mixing studies using simultaneous OH-PLIF and schlieren imaging

3. Combustion Stability Regimes of Hydrogen Jets in Supersonic Crossflow

4. 5Heltsley,W.N.,Snyder,J.A.,Mungal,M.G.,andHanson,R.K."MappingtheCombustionStability RegimesofHydrogenandHydrocarbon Jetsin Supersonic Crossflow with OH-PLIF,"14th IntSymp.on Applications ofLaserTechniques to FluidMechanics, Lisbon,Portugal, 07-10 July, 2008.

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