Modelling wall pressure fluctuations under a turbulent boundary layer
The derivation of the wave vector-frequency (w-f) spectrum of wall pressure fluctuations below a turbulent boundary layer developed over a rigid flat plate is re-considered. The Lighthill's equation for pressure fluctuations is derived in a frame of reference fix with respect to the plate, at l...
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description | The derivation of the wave vector-frequency (w-f) spectrum of wall pressure fluctuations below a turbulent boundary layer developed over a rigid flat plate is re-considered. The Lighthill's equation for pressure fluctuations is derived in a frame of reference fix with respect to the plate, at low Mach numbers, and transformed into the convected frame moving with the flow. To model the source terms of the Lighthill equation, it is assumed that in the inertial range, the turbulence is locally isotropic in the convected frame. The w-f spectrum of isotropic turbulence is obtained from symmetry considerations by extending the isotropy to space time, based on the concept of sweeping velocity. The resulting solution for the pressure w-f spectrum contains a term (the mean shear-turbulence term) which does not fulfill the Kraichnan Philipps theorem, due to the form of the selected turbulent velocity spectrum. The viscous effects are accounted for by a cut-off depending on wall distance; this procedure allows extending the model beyond the inertial range contribution. The w-f pressure spectrum is derived and compared to the experimental low wavenumber data of Farabee and Geib (1991) [8] and Bonness et al. (2010) [5], for which a good agreement is obtained. The derived expression is also compared to Chase theoretical model Chase (1987) [6] and found to agree well in the vicinity of the convective ridge of the subsonic domain and to differ significantly both in supersonic and subsonic low wavenumber limits. The pressure spectrum derived from the model and its scaling are discussed and compared to experimental data and to the empirical model of Goody (2002) [23], which results from the compilation of a large set of experimental data. Very good agreement is obtained, except at vanishing frequencies where it is claimed that the experimental results lack of significance due to the limited size of the experimental facilities. This hypothesis supported by the results obtained from numerical simulations. |
doi_str_mv | 10.1016/j.jsv.2017.04.004 |
format | Article |
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The Lighthill's equation for pressure fluctuations is derived in a frame of reference fix with respect to the plate, at low Mach numbers, and transformed into the convected frame moving with the flow. To model the source terms of the Lighthill equation, it is assumed that in the inertial range, the turbulence is locally isotropic in the convected frame. The w-f spectrum of isotropic turbulence is obtained from symmetry considerations by extending the isotropy to space time, based on the concept of sweeping velocity. The resulting solution for the pressure w-f spectrum contains a term (the mean shear-turbulence term) which does not fulfill the Kraichnan Philipps theorem, due to the form of the selected turbulent velocity spectrum. The viscous effects are accounted for by a cut-off depending on wall distance; this procedure allows extending the model beyond the inertial range contribution. The w-f pressure spectrum is derived and compared to the experimental low wavenumber data of Farabee and Geib (1991) [8] and Bonness et al. (2010) [5], for which a good agreement is obtained. The derived expression is also compared to Chase theoretical model Chase (1987) [6] and found to agree well in the vicinity of the convective ridge of the subsonic domain and to differ significantly both in supersonic and subsonic low wavenumber limits. The pressure spectrum derived from the model and its scaling are discussed and compared to experimental data and to the empirical model of Goody (2002) [23], which results from the compilation of a large set of experimental data. Very good agreement is obtained, except at vanishing frequencies where it is claimed that the experimental results lack of significance due to the limited size of the experimental facilities. This hypothesis supported by the results obtained from numerical simulations.</description><identifier>ISSN: 0022-460X</identifier><identifier>EISSN: 1095-8568</identifier><identifier>DOI: 10.1016/j.jsv.2017.04.004</identifier><language>eng</language><publisher>Amsterdam: Elsevier Ltd</publisher><subject>Accuracy ; Boundary layer ; Computational fluid dynamics ; Computer simulation ; Flat plates ; Flow noise ; Frequencies ; Isotropic turbulence ; Isotropy ; Mathematical models ; Pressure ; Studies ; Turbulence ; Turbulent boundary layer ; Variation ; Velocity ; Velocity spectrum ; Wall pressure ; Wall pressure spectrum ; Wavelengths</subject><ispartof>Journal of sound and vibration, 2017-07, Vol.400, p.178-200</ispartof><rights>2017 Elsevier Ltd</rights><rights>Copyright Elsevier Science Ltd. Jul 21, 2017</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c325t-659beff99ab9d5c0c66e0975c56ce1d2a2cddc7ca8edec34d25c70611f4436163</citedby><cites>FETCH-LOGICAL-c325t-659beff99ab9d5c0c66e0975c56ce1d2a2cddc7ca8edec34d25c70611f4436163</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0022460X17303115$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65534</link.rule.ids></links><search><creatorcontrib>Doisy, Yves</creatorcontrib><title>Modelling wall pressure fluctuations under a turbulent boundary layer</title><title>Journal of sound and vibration</title><description>The derivation of the wave vector-frequency (w-f) spectrum of wall pressure fluctuations below a turbulent boundary layer developed over a rigid flat plate is re-considered. The Lighthill's equation for pressure fluctuations is derived in a frame of reference fix with respect to the plate, at low Mach numbers, and transformed into the convected frame moving with the flow. To model the source terms of the Lighthill equation, it is assumed that in the inertial range, the turbulence is locally isotropic in the convected frame. The w-f spectrum of isotropic turbulence is obtained from symmetry considerations by extending the isotropy to space time, based on the concept of sweeping velocity. The resulting solution for the pressure w-f spectrum contains a term (the mean shear-turbulence term) which does not fulfill the Kraichnan Philipps theorem, due to the form of the selected turbulent velocity spectrum. The viscous effects are accounted for by a cut-off depending on wall distance; this procedure allows extending the model beyond the inertial range contribution. The w-f pressure spectrum is derived and compared to the experimental low wavenumber data of Farabee and Geib (1991) [8] and Bonness et al. (2010) [5], for which a good agreement is obtained. The derived expression is also compared to Chase theoretical model Chase (1987) [6] and found to agree well in the vicinity of the convective ridge of the subsonic domain and to differ significantly both in supersonic and subsonic low wavenumber limits. The pressure spectrum derived from the model and its scaling are discussed and compared to experimental data and to the empirical model of Goody (2002) [23], which results from the compilation of a large set of experimental data. Very good agreement is obtained, except at vanishing frequencies where it is claimed that the experimental results lack of significance due to the limited size of the experimental facilities. This hypothesis supported by the results obtained from numerical simulations.</description><subject>Accuracy</subject><subject>Boundary layer</subject><subject>Computational fluid dynamics</subject><subject>Computer simulation</subject><subject>Flat plates</subject><subject>Flow noise</subject><subject>Frequencies</subject><subject>Isotropic turbulence</subject><subject>Isotropy</subject><subject>Mathematical models</subject><subject>Pressure</subject><subject>Studies</subject><subject>Turbulence</subject><subject>Turbulent boundary layer</subject><subject>Variation</subject><subject>Velocity</subject><subject>Velocity spectrum</subject><subject>Wall pressure</subject><subject>Wall pressure spectrum</subject><subject>Wavelengths</subject><issn>0022-460X</issn><issn>1095-8568</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp9kE1LAzEQhoMoWKs_wFvA866TbJJ28SSlfkDFi4K3kE1mZZe4W5NNpf_elHr2NDC8z8zLQ8g1g5IBU7d92cddyYEtShAlgDghMwa1LJZSLU_JDIDzQij4OCcXMfYAUItKzMj6ZXTofTd80h_jPd0GjDEFpK1Pdkpm6sYh0jQ4DNTQKYUmeRwm2ox5Z8KeerPHcEnOWuMjXv3NOXl_WL-tnorN6-Pz6n5T2IrLqVCybrBt69o0tZMWrFII9UJaqSwyxw23ztmFNUt0aCvhuLQLUIy1QlSKqWpObo53t2H8Thgn3Y8pDPml5jkHlZKC5RQ7pmwYYwzY6m3ovnJZzUAfbOleZ1v6YEuD0NlWZu6ODOb6uw6DjrbDwaLrAtpJu7H7h_4FN1pzsQ</recordid><startdate>20170721</startdate><enddate>20170721</enddate><creator>Doisy, Yves</creator><general>Elsevier Ltd</general><general>Elsevier Science Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope></search><sort><creationdate>20170721</creationdate><title>Modelling wall pressure fluctuations under a turbulent boundary layer</title><author>Doisy, Yves</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c325t-659beff99ab9d5c0c66e0975c56ce1d2a2cddc7ca8edec34d25c70611f4436163</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Accuracy</topic><topic>Boundary layer</topic><topic>Computational fluid dynamics</topic><topic>Computer simulation</topic><topic>Flat plates</topic><topic>Flow noise</topic><topic>Frequencies</topic><topic>Isotropic turbulence</topic><topic>Isotropy</topic><topic>Mathematical models</topic><topic>Pressure</topic><topic>Studies</topic><topic>Turbulence</topic><topic>Turbulent boundary layer</topic><topic>Variation</topic><topic>Velocity</topic><topic>Velocity spectrum</topic><topic>Wall pressure</topic><topic>Wall pressure spectrum</topic><topic>Wavelengths</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Doisy, Yves</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of sound and vibration</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Doisy, Yves</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Modelling wall pressure fluctuations under a turbulent boundary layer</atitle><jtitle>Journal of sound and vibration</jtitle><date>2017-07-21</date><risdate>2017</risdate><volume>400</volume><spage>178</spage><epage>200</epage><pages>178-200</pages><issn>0022-460X</issn><eissn>1095-8568</eissn><abstract>The derivation of the wave vector-frequency (w-f) spectrum of wall pressure fluctuations below a turbulent boundary layer developed over a rigid flat plate is re-considered. The Lighthill's equation for pressure fluctuations is derived in a frame of reference fix with respect to the plate, at low Mach numbers, and transformed into the convected frame moving with the flow. To model the source terms of the Lighthill equation, it is assumed that in the inertial range, the turbulence is locally isotropic in the convected frame. The w-f spectrum of isotropic turbulence is obtained from symmetry considerations by extending the isotropy to space time, based on the concept of sweeping velocity. The resulting solution for the pressure w-f spectrum contains a term (the mean shear-turbulence term) which does not fulfill the Kraichnan Philipps theorem, due to the form of the selected turbulent velocity spectrum. The viscous effects are accounted for by a cut-off depending on wall distance; this procedure allows extending the model beyond the inertial range contribution. The w-f pressure spectrum is derived and compared to the experimental low wavenumber data of Farabee and Geib (1991) [8] and Bonness et al. (2010) [5], for which a good agreement is obtained. The derived expression is also compared to Chase theoretical model Chase (1987) [6] and found to agree well in the vicinity of the convective ridge of the subsonic domain and to differ significantly both in supersonic and subsonic low wavenumber limits. The pressure spectrum derived from the model and its scaling are discussed and compared to experimental data and to the empirical model of Goody (2002) [23], which results from the compilation of a large set of experimental data. Very good agreement is obtained, except at vanishing frequencies where it is claimed that the experimental results lack of significance due to the limited size of the experimental facilities. This hypothesis supported by the results obtained from numerical simulations.</abstract><cop>Amsterdam</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.jsv.2017.04.004</doi><tpages>23</tpages></addata></record> |
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subjects | Accuracy Boundary layer Computational fluid dynamics Computer simulation Flat plates Flow noise Frequencies Isotropic turbulence Isotropy Mathematical models Pressure Studies Turbulence Turbulent boundary layer Variation Velocity Velocity spectrum Wall pressure Wall pressure spectrum Wavelengths |
title | Modelling wall pressure fluctuations under a turbulent boundary layer |
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