Large-Eddy/Reynolds-averaged Navier-Stokes Simulation of a Dual-Mode Scramjet Combustor
Author:
Affiliation:
1. North Carolina State University
2. University of Virginia
3. The George Washington University
4. University of Calgary
5. NASA Langley Research Center
6. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-115
Reference22 articles.
1. 1McDaniel, James C., Chelliah, Harsha, and Goyne, Christopher P. "US National Center for Hypersonic Combined Cycle Propulsion: AnOverview,"AIAAPaper 2009-7280.
2. 2Wilcox,DavidC.,TurbulenceModelingforCFD,3rded.,DCWIndustries,Inc.,LaCanada,CA,2006,Sxn.1.3.2.
3. Experimental and Numerical Study of a Dual-mode Scramjet Combustor
4. 4Georgiadis, N. J. etal. "Wind-US Code Physical Modeling Improvements to Complement Hypersonic Testing and Evaluation"AIAAPaper 2009-193.
5. 5Vyas, M. A., Engblom, W. A., Georgiadis, N. J., Trefny, C. J., and Bhagwandin, V. A. "Numerical Simulation of Vitiation Effects onaHydrogen-FueledDual-ModeScramjet" AIAAPaper2010-1127.
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