Ignition and Flame Structure in a Compact Inlet/Scramjet Combustor Model-Reference-Cited by-同舟云学术

Ignition and Flame Structure in a Compact Inlet/Scramjet Combustor Model

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Gamba Mirko¹,Miller Victor¹,Mungal M. 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/10.2514/6.2011-2366

Reference16 articles.

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

2. 3Ben-Yakar, A., Kamel, M., Morris, C., and Hanson, R. K. “Hypersonic combustion and mixing studies using simultaneous OH PLIF and Schlierenimaging,”1998.

3. Combustion Stability Regimes of Hydrogen Jets in Supersonic Crossflow

4. 5Heltsley,W.N.,Snyder,J.A.,Mungal,M.G.,andHanson,R.K.“MappingtheCombustionStabilityRegimesofHydrogenandHydrocarbonJetsinSupersonicCrossflowwithOH-PLIF,”14thIntSymp.onApplicationsofLaserTechniquestoFluidMechanics,Lisbon,Portugal,07-10 July,2008.

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