Vortex Breakdown in a Swirl-Stabilized Combustor
Author:
Affiliation:
1. Nestoil PLC, Victoria Island, Lagos, Nigeria
2. Rensselaer Polytechnic Institute, Troy, New York 12180
3. University of Cincinnati, Cincinnati, Ohio 45221
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.B34377
Reference35 articles.
1. A Review of NOxFormation Under Gas-Turbine Combustion Conditions
2. Large-Eddy Simulation of Combustion Dynamics of Lean-Premixed Swirl-Stabilized Combustor
3. Proportional Control of Combustion Instabilities in a Simulated Gas-Turbine Combustor
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