Search Results for: 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
Language: en
Pages: 226

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

Authors: Sundaram C. Venkitarama
Categories: Jet planes
Type: BOOK - Published: 1981 - Publisher:

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An Acoustic Source Modeling Technique to Predict the Near Sound Field of Axisymmetric Turbulent Jets
Language: en
Pages: 77

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

Authors: J. R. Maus
Categories:
Type: BOOK - Published: 1979 - Publisher:

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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
Scientific and Technical Aerospace Reports
Language: en
Pages: 702

Scientific and Technical Aerospace Reports

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1994 - Publisher:

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Technical Abstract Bulletin
Language: en
Pages: 1048

Technical Abstract Bulletin

Authors:
Categories: Science
Type: BOOK - Published: - Publisher:

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Simulation of Supersonic Jet Noise with the Adaptation of Overflow Cfd Code and Kirchhoff Surface Integral
Language: en
Pages: 26

Simulation of Supersonic Jet Noise with the Adaptation of Overflow Cfd Code and Kirchhoff Surface Integral

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