Effects of cooling flow on the flow structure and acoustic oscillation in a swirl-stabilized combustor. Part II: Acoustic analysis
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s12650-013-0193-y.pdf
Reference20 articles.
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3. Freund JB, Colonius T (2009) Turbulence and sound-field POD analysis of a turbulent jet. Int J Aeroacoust 8(4):337–354
4. Huang Y, Wang S, Yang V (2006) Systematic analysis of lean-premixed swirl-stabilized combustion. AIAA J 44(4):724–740
5. Kim JC, Yoo KH, Sung HG (2011) Large-eddy simulation and acoustic analysis of a turbulent flow field in a swirl-stabilized combustor. J Mech Sci Tech 25(10):2703–2710
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1. LES Investigation on The Cryogenic Nitrogen Injection of Swirl Injector Under Supercritical Envionment;Journal of the Korean Society for Aeronautical & Space Sciences;2016-04-01
2. Effect of Dynamic SGS Model in a Kerosene-LOx Swirl Injector under Supercritical Condition;International Journal of Aeronautical and Space Sciences;2015-06-30
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