An Acoustic Source Modeling Technique To Predict The Near Sound Field Of Axisymmetric Turbulent Jets

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An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets

An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets
Author :
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Total Pages : 226
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ISBN-10 : OCLC:8316857
ISBN-13 :
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Book Synopsis An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets by : Sundaram C. Venkitarama

Download or read book An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets written by Sundaram C. Venkitarama and published by . This book was released on 1981 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt:


An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets Related Books

An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets
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Pages: 226
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Type: BOOK - Published: 1981 - Publisher:

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An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets
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The objective of the investigation reported herein was to develop a technique for determining the free, unreflected sound field produced by a jet engine based o
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Simulation of Supersonic Jet Noise with the Adaptation of Overflow Cfd Code and Kirchhoff Surface Integral
Language: en
Pages: 26
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-06-19 - Publisher: Createspace Independent Publishing Platform

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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