Supersonic Combustor Fuel Injection Simulations Using a Hybrid RANS/LES Approach
Author:
Affiliation:
1. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-411
Reference25 articles.
1. Quantitative investigation of compressible mixing - Staged transverse injection into Mach 2 flow
2. Velocity Measurements of a Jet Injected into a Supersonic Crossflow
3. Wall Pressure Measurements for a Sonic Jet Injected Transversely into a Supersonic Crossflow
4. Mixing of a Sonic Transverse Jet Injected into a Supersonic Flow
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