Supersonic Combustion and Flame-Holding Characteristics of Pylon Injected Hydrogen in a Mach 2.4 High Enthalpy Flow-Reference-Cited by-同舟云学术

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Supersonic Combustion and Flame-Holding Characteristics of Pylon Injected Hydrogen in a Mach 2.4 High Enthalpy Flow

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:

Vergine Fabrizio¹,Maddalena Luca¹,Miller Victor²,Gamba Mirko²

Affiliation:

1. University of Texas, Arlington

2. Stanford University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-333

Reference21 articles.

1. In-Stream Hypermixer Fueling Pylons in Supersonic Flow

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4. Vortex dynamics studies in supersonic flow: Merging of co-rotating streamwise vortices;Physics of Fluids;2014-04

5. Chemiluminescence Imaging in Supersonic Combustors Operating in Radical-Farming Mode;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

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