Influence of Sleeve Angle on the LBO Performance of TeLESS-II Combustor
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4693
Reference13 articles.
1. Gas Turbine Combustion
2. Numerical Study of the Precessing Vortex Core in a Confined Partially Premixed Swirl Combustion System
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