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... NASA/TM-2001-210263... DEC. 6,.

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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ISBN-10 : OCLC:1129331862
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SIMULATION OF SUPERSONIC JET NOISE WITH THE ADAPTATION OF OVERFLOW CFD CODE AND KIRCHHOFF SURFACE INTEGRAL... NASA/TM-2001-210263... DEC. 6,. Related Books

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
Simulation of Supersonic Jet Noise with the Adaptation of Overflow CFD Code and Kirchhoff Surface Integral
Language: en
Pages: 52
Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral
Language: en
Pages: 18