Numerical Investigation of Supersonic Injection Using a Reynolds-Stress Turbulence Model
Author:
Affiliation:
1. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7542
2. University of Alabama, Tuscaloosa, Alabama 35487
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.594
Reference36 articles.
1. Low angle injection into a supersonic flow
2. Experimental investigation of supersonic gaseous injection into a supersonic freestream
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