A Near Field Investigation of Chevron Nozzle Mechanisms
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/10.2514/6.2003-3210
Reference12 articles.
1. The distortion of a jet by tabs
2. Ahuja, K.K., Brown, W.H. "Shear FlowControl byMechanical Tabs", AIAA-89-0994,1989.
3. Effect of tabs on the flow and noise field of an axisymmetric jet
4. Ahuja, K.K., Manes, J.P.,Massey, K.C. "An EvaluationofVarious Concepts ofReducing SupersonicJet Noise", AIAA-90-3982,1990.
5. Saiyed, N.H., Bridges, J.E. "Tabs and Mixers for ReducingLowBypass Ratio Jet Noise", AIAA99-1986,1999.
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1. Impact of Chevrons on Noise Source Characteristics In Imperfectly Expanded Jet Flows;21st AIAA/CEAS Aeroacoustics Conference;2015-06-18
2. Computational Study of the Impact of Chevrons on Noise Characteristics of Imperfectly Expanded Jet Flows;52nd Aerospace Sciences Meeting;2014-01-10
3. Numerical Investigation of Fluidic Enhanced Chevrons for Noise Reduction in Supersonic Jets;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
4. CFD and CAA Analysis of Single Stream Isothermal Jets with Noise Suppression Devices;16th AIAA/CEAS Aeroacoustics Conference;2010-06-07
5. Large-Eddy Simulations of Imperfectly Expanded Jets from a Chevron Nozzle;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11
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