Large-Eddy/Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050066
Reference43 articles.
1. Interaction shock shape for transverse injection in supersonic flow
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3. Secondary injection of gases into a supersonic flow
4. Penetration of gaseous jets injected into a supersonic stream.
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