Jet Noise: Acoustic Analogy informed by Large Eddy Simulation
A novel approach to the development of a hybrid prediction methodology for jet noise is described. Modeling details and numerical techniques are optimized for each of the three components of the model. Far-field propagation is modeled by solution of a system of adjoint linear Euler equations, captur...
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creator | Karabasov, S. A Afsar, M. Z Hynes, T. P Dowling, A. P McMullan, W. A Pokora, C. D Page, G. J McGuirk, J. J |
description | A novel approach to the development of a hybrid prediction methodology for jet noise is described. Modeling details and numerical techniques are optimized for each of the three components of the model. Far-field propagation is modeled by solution of a system of adjoint linear Euler equations, capturing convective and refraction effects using a spatially developing jet mean flow provided by a Reynolds-averaged Navier-Stokes computational fluid dynamics solution. Sound generation is modeled following Goldstein's acoustic analogy, including a Gaussian function model for the two-point cross correlation of the fourth-order velocity fluctuations in the acoustic source. Parameters in this model describing turbulent length and time scales are assumed to be proportional to turbulence information also taken from the Reynolds-averaged Navier-Stokes computational fluid dynamics prediction. The constants of proportionality are, however, not determined empirically, but extracted by comparison with turbulence length and time scales obtained from a large eddy simulation prediction. The large eddy simulation results are shown to be in good agreement with experimental data for the fourth-order two-point cross-correlation functions. The large eddy simulation solution is then used to determine the amplitude parameter and also to examine which components of the cross correlation are largest, enabling inclusion of all identified dominant terms in the Gaussian source model. The acoustic source description in the present approach is therefore determined with no direct input from experimental data. This model is applied to the prediction of sound to the experimental configuration of the European Union JEAN project, and gives encouraging agreement with experimental data across a wide spectral range and for both sideline and peak noise angles. This paper also examines the accuracy of various commonly made simplifications, for example: a locally parallel mean flow approximation rather than consideration of the spatially evolving mean jet flow and scattering from the nozzle; the assumption of small radial variation in Green function over the turbulence correlation length; the application of the far-field approximation in the Green function; and the impact of isotropic assumptions made in previous acoustic source models. [PUBLICATION ABSTRACT] |
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A ; Afsar, M. Z ; Hynes, T. P ; Dowling, A. P ; McMullan, W. A ; Pokora, C. D ; Page, G. J ; McGuirk, J. J</creator><creatorcontrib>Karabasov, S. A ; Afsar, M. Z ; Hynes, T. P ; Dowling, A. P ; McMullan, W. A ; Pokora, C. D ; Page, G. J ; McGuirk, J. J</creatorcontrib><description>A novel approach to the development of a hybrid prediction methodology for jet noise is described. Modeling details and numerical techniques are optimized for each of the three components of the model. Far-field propagation is modeled by solution of a system of adjoint linear Euler equations, capturing convective and refraction effects using a spatially developing jet mean flow provided by a Reynolds-averaged Navier-Stokes computational fluid dynamics solution. Sound generation is modeled following Goldstein's acoustic analogy, including a Gaussian function model for the two-point cross correlation of the fourth-order velocity fluctuations in the acoustic source. Parameters in this model describing turbulent length and time scales are assumed to be proportional to turbulence information also taken from the Reynolds-averaged Navier-Stokes computational fluid dynamics prediction. The constants of proportionality are, however, not determined empirically, but extracted by comparison with turbulence length and time scales obtained from a large eddy simulation prediction. The large eddy simulation results are shown to be in good agreement with experimental data for the fourth-order two-point cross-correlation functions. The large eddy simulation solution is then used to determine the amplitude parameter and also to examine which components of the cross correlation are largest, enabling inclusion of all identified dominant terms in the Gaussian source model. The acoustic source description in the present approach is therefore determined with no direct input from experimental data. This model is applied to the prediction of sound to the experimental configuration of the European Union JEAN project, and gives encouraging agreement with experimental data across a wide spectral range and for both sideline and peak noise angles. This paper also examines the accuracy of various commonly made simplifications, for example: a locally parallel mean flow approximation rather than consideration of the spatially evolving mean jet flow and scattering from the nozzle; the assumption of small radial variation in Green function over the turbulence correlation length; the application of the far-field approximation in the Green function; and the impact of isotropic assumptions made in previous acoustic source models. 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A</creatorcontrib><creatorcontrib>Afsar, M. Z</creatorcontrib><creatorcontrib>Hynes, T. P</creatorcontrib><creatorcontrib>Dowling, A. P</creatorcontrib><creatorcontrib>McMullan, W. A</creatorcontrib><creatorcontrib>Pokora, C. D</creatorcontrib><creatorcontrib>Page, G. J</creatorcontrib><creatorcontrib>McGuirk, J. J</creatorcontrib><title>Jet Noise: Acoustic Analogy informed by Large Eddy Simulation</title><title>AIAA journal</title><description>A novel approach to the development of a hybrid prediction methodology for jet noise is described. Modeling details and numerical techniques are optimized for each of the three components of the model. Far-field propagation is modeled by solution of a system of adjoint linear Euler equations, capturing convective and refraction effects using a spatially developing jet mean flow provided by a Reynolds-averaged Navier-Stokes computational fluid dynamics solution. Sound generation is modeled following Goldstein's acoustic analogy, including a Gaussian function model for the two-point cross correlation of the fourth-order velocity fluctuations in the acoustic source. Parameters in this model describing turbulent length and time scales are assumed to be proportional to turbulence information also taken from the Reynolds-averaged Navier-Stokes computational fluid dynamics prediction. The constants of proportionality are, however, not determined empirically, but extracted by comparison with turbulence length and time scales obtained from a large eddy simulation prediction. The large eddy simulation results are shown to be in good agreement with experimental data for the fourth-order two-point cross-correlation functions. The large eddy simulation solution is then used to determine the amplitude parameter and also to examine which components of the cross correlation are largest, enabling inclusion of all identified dominant terms in the Gaussian source model. The acoustic source description in the present approach is therefore determined with no direct input from experimental data. This model is applied to the prediction of sound to the experimental configuration of the European Union JEAN project, and gives encouraging agreement with experimental data across a wide spectral range and for both sideline and peak noise angles. This paper also examines the accuracy of various commonly made simplifications, for example: a locally parallel mean flow approximation rather than consideration of the spatially evolving mean jet flow and scattering from the nozzle; the assumption of small radial variation in Green function over the turbulence correlation length; the application of the far-field approximation in the Green function; and the impact of isotropic assumptions made in previous acoustic source models. [PUBLICATION ABSTRACT]</description><subject>Accuracy</subject><subject>Acoustic sources</subject><subject>Acoustics</subject><subject>Aeroacoustics, atmospheric sound</subject><subject>Aircraft</subject><subject>Analogies</subject><subject>Approximation</subject><subject>Computational fluid dynamics</subject><subject>Computational methods in fluid dynamics</subject><subject>Constants</subject><subject>Correlation</subject><subject>Cross correlation</subject><subject>Dynamical systems</subject><subject>Eulers equations</subject><subject>European union</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fluid flow</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Gaussian</subject><subject>Green's functions</subject><subject>Inclusions</subject><subject>Jet flow</subject><subject>Jet noise</subject><subject>Large eddy simulation</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Methodology</subject><subject>Navier-Stokes equations</subject><subject>Noise</subject><subject>Noise (turbulence generated)</subject><subject>Nozzles</subject><subject>Physics</subject><subject>Refraction</subject><subject>Scattering</subject><subject>Simulation</subject><subject>Sound</subject><subject>Spectra</subject><subject>Turbulence</subject><subject>Turbulence simulation and modeling</subject><subject>Turbulent flow</subject><subject>Turbulent flows, convection, and heat transfer</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><recordid>eNptkN9LwzAQx4MoOKf4LxRRxIfOJmmaVPBhjPmLoQ8q-BauaTIyunYmLdj_3uiGA_XpOO7D5-6-CB3jZEQYTi_xKE0zke-gAWaUxlSwt100SJIExzhlZB8deL8IHeECD9D1g26jx8Z6fRWNVdP51qpoXEPVzPvI1qZxS11GRR_NwM11NC3LPnq2y66C1jb1IdozUHl9tKlD9HozfZncxbOn2_vJeBYD5byNFSjOABNcFgwLxtM05YXgtDAFVapkOc-BC5OCzrQgVIjcFGX4hUGRF5xoOkTna-_KNe-d9q1cWq90VUGtw82SM5plSZ6TQJ78IhdN58I_XjLOieA8IVudco33Thu5cnYJrpc4kV8hSiy_Qwzk2UYHXkFlHNTK-h-c0CQosQjc6ZoDC7Bd-Vd38S-2HstVaaTpqqrVHy39BD8jiG0</recordid><startdate>20100701</startdate><enddate>20100701</enddate><creator>Karabasov, S. A</creator><creator>Afsar, M. Z</creator><creator>Hynes, T. P</creator><creator>Dowling, A. P</creator><creator>McMullan, W. A</creator><creator>Pokora, C. D</creator><creator>Page, G. J</creator><creator>McGuirk, J. J</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20100701</creationdate><title>Jet Noise: Acoustic Analogy informed by Large Eddy Simulation</title><author>Karabasov, S. A ; Afsar, M. Z ; Hynes, T. P ; Dowling, A. P ; McMullan, W. A ; Pokora, C. D ; Page, G. J ; McGuirk, J. 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J</au><au>McGuirk, J. J</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Jet Noise: Acoustic Analogy informed by Large Eddy Simulation</atitle><jtitle>AIAA journal</jtitle><date>2010-07-01</date><risdate>2010</risdate><volume>48</volume><issue>7</issue><spage>1312</spage><epage>1325</epage><pages>1312-1325</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>A novel approach to the development of a hybrid prediction methodology for jet noise is described. Modeling details and numerical techniques are optimized for each of the three components of the model. Far-field propagation is modeled by solution of a system of adjoint linear Euler equations, capturing convective and refraction effects using a spatially developing jet mean flow provided by a Reynolds-averaged Navier-Stokes computational fluid dynamics solution. Sound generation is modeled following Goldstein's acoustic analogy, including a Gaussian function model for the two-point cross correlation of the fourth-order velocity fluctuations in the acoustic source. Parameters in this model describing turbulent length and time scales are assumed to be proportional to turbulence information also taken from the Reynolds-averaged Navier-Stokes computational fluid dynamics prediction. The constants of proportionality are, however, not determined empirically, but extracted by comparison with turbulence length and time scales obtained from a large eddy simulation prediction. The large eddy simulation results are shown to be in good agreement with experimental data for the fourth-order two-point cross-correlation functions. The large eddy simulation solution is then used to determine the amplitude parameter and also to examine which components of the cross correlation are largest, enabling inclusion of all identified dominant terms in the Gaussian source model. The acoustic source description in the present approach is therefore determined with no direct input from experimental data. This model is applied to the prediction of sound to the experimental configuration of the European Union JEAN project, and gives encouraging agreement with experimental data across a wide spectral range and for both sideline and peak noise angles. This paper also examines the accuracy of various commonly made simplifications, for example: a locally parallel mean flow approximation rather than consideration of the spatially evolving mean jet flow and scattering from the nozzle; the assumption of small radial variation in Green function over the turbulence correlation length; the application of the far-field approximation in the Green function; and the impact of isotropic assumptions made in previous acoustic source models. [PUBLICATION ABSTRACT]</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.44689</doi><tpages>14</tpages></addata></record> |
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subjects | Accuracy Acoustic sources Acoustics Aeroacoustics, atmospheric sound Aircraft Analogies Approximation Computational fluid dynamics Computational methods in fluid dynamics Constants Correlation Cross correlation Dynamical systems Eulers equations European union Exact sciences and technology Fluid dynamics Fluid flow Fundamental areas of phenomenology (including applications) Gaussian Green's functions Inclusions Jet flow Jet noise Large eddy simulation Mathematical analysis Mathematical models Methodology Navier-Stokes equations Noise Noise (turbulence generated) Nozzles Physics Refraction Scattering Simulation Sound Spectra Turbulence Turbulence simulation and modeling Turbulent flow Turbulent flows, convection, and heat transfer |
title | Jet Noise: Acoustic Analogy informed by Large Eddy Simulation |
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