Fuel-vortex interactions for enhanced mixing in supersonic flow
Author:
Affiliation:
1. USAF; Taitech, Inc., Wright-Patterson AFB, OH
2. USAF, Wright Lab., Wright-Patterson AFB, OH
3. Virginia Polytechnic Inst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2661
Reference33 articles.
1. Penetration of gaseous jets injected into a supersonic stream.
2. Structure of highly underexpanded transverse jets in a supersonic stream.
3. Supersonic transverse injection into a supersonic stream.
4. Interaction shock shape for transverse injection in supersonic flow
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