Mixing and combustion in scramjet combustor with raised and relieved ramp
Author:
Affiliation:
1. Old Dominion Univ., Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3709
Reference30 articles.
1. Analysis of losses in supersonic mixing and reacting flows
2. Vorticity generation mechanisms in parallel injection schemes for supersonic mixing
3. Nickol, C. L. "Unswept Ramp Fuel Injector Base Aspect Ratio Parametric Study inaMach 2.9Freestream", M.Sc. Thesis,University of Virginia, Charlottesville,VA,1994.
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1. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.;22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference;2018-09-15
2. Numerical Simulation of Ethylene Injection from In-stream Fueling Pylons;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28
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