Flame Stability Analysis in an Ultra Compact Combustor Using Large-Eddy Simulation
Author:
Affiliation:
1. University of Texas, Austin
2. Oregon State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1022
Reference26 articles.
1. Turbulent combustion in a curving, contracting channel with a cavity stabilized flame
2. Gas Turbine Combustion
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4. Design Studies of Turbine Blade Film Cooling With Unburned Fuel in Cross-Stream Flow
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2. LES of a sooting flame in a pressurized swirl combustor;54th AIAA Aerospace Sciences Meeting;2016-01-02
3. Numerical Study on Flame Stabilization Mechanism of a multi-jet burner with LES Flamelet Approach;54th AIAA Aerospace Sciences Meeting;2016-01-02
4. Analytic Rayleigh pressure loss model for high-swirl combustion in a rotating combustion chamber;CEAS Aeronautical Journal;2015-10-05
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