Simulation Of Supersonic Jet Noise With The Adaptation Of Overflow Cfd Code And Kirchhoff Surface Integral Nasa Tm 2001 210263 Dec 6

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Simulation of Supersonic Jet Noise with the Adaptation of Overflow Cfd Code and Kirchhoff Surface Integral
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Authors: National Aeronautics and Space Administration (NASA)
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An acoustic prediction capability for supersonic axisymmetric jets was developed on the basis of OVERFLOW Navier-Stokes CFD (Computational Fluid Dynamics) code
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An extensive analysis of our jet DNS database has provided for the first time the complex correlations that are the core of many statistical jet noise models, i
The Generation and Radiation of Supersonic Jet Noise
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This document describes the development of an improved predictive model for coannular jet noise, including noise suppression modifications applicable to small s