DES Investigation of Transverse Injection into Supersonic Crossflow using a Hybrid Unstructured Solver
Author:
Affiliation:
1. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-903
Reference27 articles.
1. Historical Survey on Enhanced Mixing in Scramjet Engines
2. Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice into Supersonic Flow
3. Sonic Injection from Diamond-Shaped Orifices into a Supersonic Crossflow
4. Sonic Injection into a Mach 5.0 Freestream Through Diamond Orifices
5. Progress towards hybrid RANS-LES modeling for high-speed jet flows
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3. Numerical Investigation of a Supersonic Cavity Flameholder;52nd Aerospace Sciences Meeting;2014-01-10
4. Simulations of Mixing in an Inlet-Fueled Axisymmetric Scramjet;AIAA Journal;2013-12
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