Dual Mode Scramjet Combustor: Analysis of Two Configurations
Author:
Affiliation:
1. Taitech, inc.
2. U.S. Air Force Research Laboratory
3. Innovatie Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-751
Reference12 articles.
1. A Century of Ramjet Propulsion Technology Evolution
2. Pratt,D.T."Isolator-CombustorInteractioninaDual-ModeScramjetEngine,"AIAA-93-0358,1993.
3. Mathur, T., and Streby, G. "Supersonic Combustion Experiments with a Cavity-Based Fuel Injector," AIAA99-2102,1999.
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