The Behavior of an Ultra-Compact Combustor (UCC) Based on Centrifugally-Enhanced Turbulent Burning Rates
Author:
Affiliation:
1. Air Force Research Laboratory
2. Innovative Scientific Solutions Inc
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3541
Reference13 articles.
1. Selected challenges in jet and rocket engine combustion research
2. Performance Increases for Gas-Turbine Engines Through Combustion Inside the Turbine
3. Turbojet and turbofan engine performance increases through turbine burners
4. Zelina, J., Ehret, J., Hancock, R. D., Shouse, D. T., Sturgess, G. J., and Roquemore, W. M. "Ultra-Compact Combustion Technology Using High Swirl to Enhance BurningRate," AIAA2002-3725.
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