Effects of Inlet Distortion on Cavity Ignition in Supersonic Flow
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0882
Reference13 articles.
1. Studies of Inlet Distortion in a Direct-Connect Axisymmetric Scramjet Isolator
2. 2Hagenmaier, M. A., Eklund, D. R., and Milligan, R. T. "Improved Simulation of Inflow Distortion for Direct-Connect Scramjet Studies," AIAA-2011-233.
3. 3Gruber, M. R., Hagenmaier, M. A., and Mathur, T. "Simulating Inlet Distortion Effects in a Direct-Connect Scramjet Combustor," AIAA-2006-4680.
4. 4Tam, C.J., Hsu, K.Y., Hagenmaier, M., and Raffoul, C. "Simulations of Inlet Distortion Effects in a Direct-Connect Scramjet Isolator," AIAA-2011-5540.
5. 5Boles, J., Milligan, R., Hagenmaier, M., Carter, C., and Donbar, J. "Effect of Flow Distortion on Cavity-Assisted Fuel Injection," AIAA-2012-4000.
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