Affiliation:
1. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. Mixing of a Sonic Transverse Jet Injected into a Supersonic Flow
2. 2Peterson, D.M., and Candler, G.V. “Supersonic Combustor Fuel Injection Simulations Using a Hybrid rans/les Approach,” AIAA Paper No. 2010-411.
3. Hybrid Reynolds-Averaged and Large-Eddy Simulation of Normal Injection into a Supersonic Crossflow
4. 4Peterson, D.M., and Candler, G.V. “Hybrid rans/les of a Supersonic Combustor,” AIAA Paper No. 2008-6923.
5. 5Peterson, D.M., Candler, G.V., and Drayna, T.W.“Detached Eddy Simulation of a Generic Scramjet Inlet and Combustor,” AIAA Paper No. 2009-130.
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