A Far-Field Acoustic Investigation into Chevron Node Mechanisms and Trends
Author:
Affiliation:
1. University of Cincinnati
2. General Electric Aircraft Engines
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1058
Reference18 articles.
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2. Ahuja,K.K.,Manes,J.P., Massey,K.C. "AnEvaluationofVariousConceptsof ReducingSupersoNcJetNoise",AIAA-90-3982, 1990.
3. Saiyed, N.H., Bridges,J.E. "Tabsand MixersforReducingLowBypassRatioJet Noise",AIAA-99-1986, 1999.
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1. Comparison of RANS-based methods for the prediction of noise emitted by subsonic turbulent jets;19th AIAA/CEAS Aeroacoustics Conference;2013-05-24
2. Broadband Shock Associated Noise Suppression by Chevrons;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
3. A PIV Flow Field Investigation of Chevron Nozzle Mechanisms;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05
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