Comparison of Open and Choked Premixed Combustor Exits During Thermoacoustic Limit Cycle
Author:
Affiliation:
1. University of Melbourne, Melbourne, Victoria 3010, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.32650
Reference28 articles.
1. Modeling Premixed Combustion-Acoustic Wave Interactions: A Review
2. Low-frequency combustion oscillations in a model afterburner☆
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