Analysis of dual-mode hydrocarbon scramjet operation at Mach 4-6.5
Author:
Affiliation:
1. Taitech, Inc., Beavercreek, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3299
Reference37 articles.
1. Jackson, K. R., Gruber, M. R., Mathur, T. Streby, G., Smith, C. and Billig, F. "Calibration of a Newly Developed Direct-Connect High-Enthalpy Supersonic Combustion Research Facility". AIAA Paper 98-1510, April 1998.
2. Baurle, R. A., Tarn C.J., and Dasgupta, S. "Analysis of Unsteady Cavity Flows for Scramjet Applications". AIAA Paper 2000-3617, July 2000.
3. Rodriguez, C. G., White, J. A., and Riggins, D. W. "Three-Dimensional Effects in Modeling of Dual Mode Scramjets". AIAA Paper 2000-3704, July 2000.
4. Eklund, D. R., Baurle, R. A., and Gruber, M. R. "Computational Study of a Supersonic Combustor Fueled by an Aerodynamic Ramp Injector". AIAA Paper 2001-0379, Jan.2001.
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