Flow Distortion: Computational Investigation of a Shocked Cavity Flameholder
Author:
Affiliation:
1. Taitech, Inc.
2. Air Force Research Laboratory
3. Innovative Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2838
Reference12 articles.
1. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors
2. Collatz, M. J., Gruber, M. R.,Olmstead, D. T.,Branam, R. D., Lin, K-C., and Tam, C-J, "Dual Cavity Scramjet Operabilityand Performance Study," AIAA2009-5030,2009.
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