Mixing and Combustion Studies Using Cavity-Based Flameholders in a Supersonic Flow
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
2. Innovative Scientific Solutions, Inc., Dayton, Ohio 45440
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5360
Reference15 articles.
1. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
2. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors
3. Experimental investigation on dual-purpose cavity in supersonic reacting flows
4. Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor
5. Effect of Flame-Holding Cavities on Supersonic-Combustion Performance
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