Intermittent Burst Oscillations: Signature Prior to Flame Blowout in a Turbulent Swirl-Stabilized Combustor
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600 036, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35526
Reference48 articles.
1. Interaction of heat release and vortex breakdown during flame flashback driven by combustion induced vortex breakdown
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4. Swirler Flow Field Characteristics in a Sudden Expansion Combustor Geometry
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