Modeling Scramjet Flows with Variable Turbulent Prandtl and Schmidt Numbers
Author:
Affiliation:
1. North Carolina State University
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-128
Reference17 articles.
1. Numerical study of a scramjet combustor fueled by an aerodynamic ramp injector in dual-mode combustion
2. A Variable Turbulent Schmidt Number Formulation for Scramjet Application
3. Role of Turbulent Prandtl Number on Heat Flux at Hypersonic Mach Numbers
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