Simulation of transverse gas injection in turbulent supersonic air flows
Author:
Affiliation:
1. University of Rome "La Sapienza", 00184 Rome, Italy
2. University of Reggio Calabria, 89128 Reggio Calabria, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12332
Reference22 articles.
1. Numerical Study of a Scramjet Engine Flowfield
2. Numerical Study of Staged Fuel Injection for Supersonic Combustion
3. Numerical study of chemically reacting flows using a lower-upper symmetric successive overrelaxation scheme
4. A critical evaluation of two-equation models for near wall turbulence
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