Flame Stabilization in Small Cavities
Author:
Affiliation:
1. University of Dayton Research Institute, Dayton, Ohio 45469
2. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433
3. Innovative Scientific Solutions, Inc., Dayton, Ohio 45440
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.44162
Reference33 articles.
1. The Behavior of an Ultra-Compact Combustor (UCC) Based on Centrifugally-Enhanced Turbulent Burning Rates
2. Computational Analysis of the Ultra Compact Combustor
3. Compact Combustion Systems Using a Combination of Trapped Vortex and High-G Combustor Technologies
4. Ultra-Compact Combustion Technology Using High Swirl for Enhanced Burning Rate
5. The Behavior of an Ultra-Compact Combustor (UCC) Based on Centrifugally-Enhanced Turbulent Burning Rates
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