A Variable Turbulent Schmidt Number Formulation for Scramjet Application
Author:
Affiliation:
1. North Carolina State University
2. George Washington University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1099
Reference7 articles.
1. 1Eklund, D. R., Baurle, R. A., and Gruber, M. R. "Numerical Study of a Scramjet Combustor Fueled by an Aerodynamic Ramp Injector in Dual-ModeCombustion,"AIAAPaper 2001-0379, January2001.
2. 2Cutler, A. D., Diskin, G. S., Danehy, P. M., and Drummond, J. P. "Fundamental Mixing and Combustion Experiments for Propelled HypersonicFlight,"AIAAPaper AIAA-2002-3879, July2002.
3. 3Cutler, A. D., Carty, A. A., Doemer, S. E., Diskin, G. S., and Drummond, J. P. "Supersonic Coaxial Jet Flow Experiment for CFDCodeValidation,"AIAAPaper AIAA-99-3588, July1999 .
4. Further Development of the k-? (Enstrophy) Turbulence Closure Model
5. 5Girimaji, S. S. "A Simple Recipe for Modeling Reaction-Rates in Flows with Turbulent-Combustion," AIAA Paper 91-1792, June1991.
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