Study on trapped-vortex combustor - Effect of injection on dynamics of non-reacting and reacting flows in a cavity
Author:
Affiliation:
1. Innovative Scientific Solutions, Inc., Dayton, OH
2. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3256
Reference12 articles.
1. Hsu, K. Y., Goss, L. P., Trump, D. D., and Roquemore, W. M., 1995, "Performance of a Trapped-Vortex Combustor,"AIAAPaper 95-0810,Washington, D. C., Jan. 9-12.
2. Rohsenow, W. M., Fink, C. H., and Pollis, S. R., 1951, "Flow Through Two Orifices in Series," American Society of Mechanical Engineers Paper No. 51-A-87.
3. The Effect of a Rear-Mounted Disc on the Drag of a Blunt-Based Body of Revolution
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