Numerical Prediction of Chevron Nozzle Noise Reduction Using Wind-MGBK Methodology
Author:
Affiliation:
1. NASA Glenn Research Center
2. QSS/NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2979
Reference16 articles.
1. Acoustics and thrust of separate-flow exhaust nozzles with mixing devices for high-bypass-ratio engines
2. Birch, S.F., Lyubimov, D.A., Secundov, A.N., and Yakubovsky, K.Y. "Numerical Modeling Requirements for Coaxial and Chevron Nozzle Flows," AIAA-2003-3287, May2003.
3. Thomas, R.H., Kinzie, K.W., and Pao, S.P. "Computational Analysis of a Pylon-chevron Core Nozzle Interaction," AIAA-2001-2185, May2001.
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