Effects of Perforated Liners on Controlling Combustion Instabilities in Annular Combustors
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference43 articles.
1. StruttJ. W.RayleighS. B., The Theory of Sound, Vol. 2, Macmillan, New York, 1896, pp. 224–234.
2. Prediction and control of combustion instabilities in real engines
3. A review of acoustic dampers applied to combustion chambers in aerospace industry
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