Dual-Mode Scramjet Combustor: Numerical Sensitivity and Evaluation of Experiments
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/10.2514/6.2012-947
Reference13 articles.
1. Newly Developed Direct-Connect High-Enthalpy Supersonic Combustion Research Facility
2. Milligan, R., Eklund, D., Wolff, J. M., Gruber, M.,and Mathur, T."Dual Mode Scramjet Combustor: Analysis ofTwo Configurations," AIAA-2010-751.
3. Combustor Operability and Performance Verification for HIFiRE Flight 2
4. Sturgess, G.J., and McManus, K.R. "CalculationsofTurbulent MassTransport ina Bluff-BodyDiffusion-Flame Combustor," AIAA-84-0372.
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