Large Eddy Simulation Analysis of Flow Field Inside a High-g Combustor
Author:
Affiliation:
1. University of Texas, Austin
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1140
Reference26 articles.
1. 1S. Lukachko, D. Kirk, I. Waitz, Gas turbine engine durability impacts of high fuel-air ratio combustors - part 1: Potential for secondary combustion of partially reacted fuel, Journal of Engineering for Gas Turbines and Power 125 (2003) 742-750.
2. 2D. Kirk, G. Guenette, S. Lukachko, I. Waitz, Gas turbine engine durability impacts of high fuel-air ratio combustorspart ii: Near-wall reaction e↵ects on film-cooled heat transfer, Journal of Engineering for Gas Turbines and Power 125 (2003) 751-759.
3. 3W. S. Anderson, M. D. Polanka, J. Zelina, D. S. Evans, S. D. Stou↵er, G. R. Justinger, E↵ects of a reacting cross-stream on turbine film cooling, Journal of Engineering for Gas Turbines and Power 132 (5) (2010) 051501. URL http://link.aip.org/link/?GTP/132/051501/1
4. 4A. M. Briones, J. Zelina, V. R. Katta, Flame Stabilization in Small Cavities, AIAA Journal 48 (2010) 224-235.
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