On the performance of WENO/TENO schemes to resolve turbulence in DNS/LES of high‐speed compressible flows
Summary High‐speed compressible turbulent flows typically contain discontinuities and have been widely modeled using Weighted Essentially Non‐Oscillatory (WENO) schemes due to their high‐order accuracy and sharp shock capturing capability. However, such schemes may damp the small scales of turbulenc...
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Veröffentlicht in: | International journal for numerical methods in fluids 2021-01, Vol.93 (1), p.176-196 |
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description | Summary
High‐speed compressible turbulent flows typically contain discontinuities and have been widely modeled using Weighted Essentially Non‐Oscillatory (WENO) schemes due to their high‐order accuracy and sharp shock capturing capability. However, such schemes may damp the small scales of turbulence and result in inaccurate solutions in the context of turbulence‐resolving simulations. In this connection, the recently developed Targeted Essentially Non‐Oscillatory (TENO) schemes, including adaptive variants, may offer significant improvements. The present study aims to quantify the potential of these new schemes for a fully turbulent supersonic flow. Specifically, DNS of a compressible turbulent channel flow with M = 1.5 and Reτ = 222 is conducted using OpenSBLI, a high‐order finite difference computational fluid dynamics framework. This flow configuration is chosen to decouple the effect of flow discontinuities and turbulence and focus on the capability of the aforementioned high‐order schemes to resolve turbulent structures. The effect of the spatial resolution in different directions and coarse grid implicit LES are also evaluated against the WALE LES model. The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. Although the most computationally expensive scheme, it is shown that this adaptive scheme can produce satisfactory results if used as an implicit LES model.
The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. The adaptive TENO scheme can produce satisfactory results if used as an implicit LES model. |
doi_str_mv | 10.1002/fld.4879 |
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High‐speed compressible turbulent flows typically contain discontinuities and have been widely modeled using Weighted Essentially Non‐Oscillatory (WENO) schemes due to their high‐order accuracy and sharp shock capturing capability. However, such schemes may damp the small scales of turbulence and result in inaccurate solutions in the context of turbulence‐resolving simulations. In this connection, the recently developed Targeted Essentially Non‐Oscillatory (TENO) schemes, including adaptive variants, may offer significant improvements. The present study aims to quantify the potential of these new schemes for a fully turbulent supersonic flow. Specifically, DNS of a compressible turbulent channel flow with M = 1.5 and Reτ = 222 is conducted using OpenSBLI, a high‐order finite difference computational fluid dynamics framework. This flow configuration is chosen to decouple the effect of flow discontinuities and turbulence and focus on the capability of the aforementioned high‐order schemes to resolve turbulent structures. The effect of the spatial resolution in different directions and coarse grid implicit LES are also evaluated against the WALE LES model. The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. Although the most computationally expensive scheme, it is shown that this adaptive scheme can produce satisfactory results if used as an implicit LES model.
The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. The adaptive TENO scheme can produce satisfactory results if used as an implicit LES model.</description><identifier>ISSN: 0271-2091</identifier><identifier>EISSN: 1097-0363</identifier><identifier>DOI: 10.1002/fld.4879</identifier><language>eng</language><publisher>Hoboken, USA: John Wiley & Sons, Inc</publisher><subject>Accuracy ; Channel flow ; code generation ; Compressible flow ; Computational fluid dynamics ; Computer applications ; Discontinuity ; Finite difference method ; Fluid dynamics ; Fluid flow ; GPU ; high order ; Hydrodynamics ; OpenSBLI ; Resolution ; Shock capturing ; Spatial discrimination ; Spatial resolution ; Spectral methods ; Statistical methods ; Supersonic flow ; TENO ; Turbulence ; Turbulent flow</subject><ispartof>International journal for numerical methods in fluids, 2021-01, Vol.93 (1), p.176-196</ispartof><rights>2020 The Authors. published by John Wiley & Sons, Ltd.</rights><rights>2020. This article is published under http://creativecommons.org/licenses/by/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4309-26a2ba6648a4c4ffcb7248eb765dca56b734766dc82bbbdc2cfcc5ef56f162a03</citedby><cites>FETCH-LOGICAL-c4309-26a2ba6648a4c4ffcb7248eb765dca56b734766dc82bbbdc2cfcc5ef56f162a03</cites><orcidid>0000-0003-1470-4490</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Ffld.4879$$EPDF$$P50$$Gwiley$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Ffld.4879$$EHTML$$P50$$Gwiley$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,1411,27901,27902,45550,45551</link.rule.ids></links><search><creatorcontrib>Hamzehloo, Arash</creatorcontrib><creatorcontrib>Lusher, David J.</creatorcontrib><creatorcontrib>Laizet, Sylvain</creatorcontrib><creatorcontrib>Sandham, Neil D.</creatorcontrib><title>On the performance of WENO/TENO schemes to resolve turbulence in DNS/LES of high‐speed compressible flows</title><title>International journal for numerical methods in fluids</title><description>Summary
High‐speed compressible turbulent flows typically contain discontinuities and have been widely modeled using Weighted Essentially Non‐Oscillatory (WENO) schemes due to their high‐order accuracy and sharp shock capturing capability. However, such schemes may damp the small scales of turbulence and result in inaccurate solutions in the context of turbulence‐resolving simulations. In this connection, the recently developed Targeted Essentially Non‐Oscillatory (TENO) schemes, including adaptive variants, may offer significant improvements. The present study aims to quantify the potential of these new schemes for a fully turbulent supersonic flow. Specifically, DNS of a compressible turbulent channel flow with M = 1.5 and Reτ = 222 is conducted using OpenSBLI, a high‐order finite difference computational fluid dynamics framework. This flow configuration is chosen to decouple the effect of flow discontinuities and turbulence and focus on the capability of the aforementioned high‐order schemes to resolve turbulent structures. The effect of the spatial resolution in different directions and coarse grid implicit LES are also evaluated against the WALE LES model. The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. Although the most computationally expensive scheme, it is shown that this adaptive scheme can produce satisfactory results if used as an implicit LES model.
The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. The adaptive TENO scheme can produce satisfactory results if used as an implicit LES model.</description><subject>Accuracy</subject><subject>Channel flow</subject><subject>code generation</subject><subject>Compressible flow</subject><subject>Computational fluid dynamics</subject><subject>Computer applications</subject><subject>Discontinuity</subject><subject>Finite difference method</subject><subject>Fluid dynamics</subject><subject>Fluid flow</subject><subject>GPU</subject><subject>high order</subject><subject>Hydrodynamics</subject><subject>OpenSBLI</subject><subject>Resolution</subject><subject>Shock capturing</subject><subject>Spatial discrimination</subject><subject>Spatial resolution</subject><subject>Spectral methods</subject><subject>Statistical methods</subject><subject>Supersonic flow</subject><subject>TENO</subject><subject>Turbulence</subject><subject>Turbulent flow</subject><issn>0271-2091</issn><issn>1097-0363</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>24P</sourceid><recordid>eNp10LFOwzAQBmALgUQpSDyCJRaWtI6T2MmISgtIUTu0iDGynTNJSeJgN1TdeASekSchoawsd8v330k_Qtc-mfiE0Kmu8kkY8-QEjXyScI8ELDhFI0K571GS-OfowrktISShcTBCb6sG7wrALVhtbC0aBdho_DJfrqabfmCnCqjB4Z3BFpypPgDvOiu7CgZaNvh-uZ6m8_WQKsrX4vvzy7UAOVambvuEK2UFWFdm7y7RmRaVg6u_PUbPi_lm9uilq4en2V3qqTAgiUeZoFIwFsYiVKHWSnIaxiA5i3IlIiZ5EHLGchVTKWWuqNJKRaAjpn1GBQnG6OZ4t7XmvQO3y7ams03_MqMhY5ySgCe9uj0qZY1zFnTW2rIW9pD5JBuqzPoqs6HKnnpHui8rOPzrskV6_-t_AFfddgA</recordid><startdate>202101</startdate><enddate>202101</enddate><creator>Hamzehloo, Arash</creator><creator>Lusher, David J.</creator><creator>Laizet, Sylvain</creator><creator>Sandham, Neil D.</creator><general>John Wiley & Sons, Inc</general><general>Wiley Subscription Services, Inc</general><scope>24P</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QH</scope><scope>7SC</scope><scope>7TB</scope><scope>7U5</scope><scope>7UA</scope><scope>8FD</scope><scope>C1K</scope><scope>F1W</scope><scope>FR3</scope><scope>H8D</scope><scope>H96</scope><scope>JQ2</scope><scope>KR7</scope><scope>L.G</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0003-1470-4490</orcidid></search><sort><creationdate>202101</creationdate><title>On the performance of WENO/TENO schemes to resolve turbulence in DNS/LES of high‐speed compressible flows</title><author>Hamzehloo, Arash ; Lusher, David J. ; Laizet, Sylvain ; Sandham, Neil D.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c4309-26a2ba6648a4c4ffcb7248eb765dca56b734766dc82bbbdc2cfcc5ef56f162a03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Accuracy</topic><topic>Channel flow</topic><topic>code generation</topic><topic>Compressible flow</topic><topic>Computational fluid dynamics</topic><topic>Computer applications</topic><topic>Discontinuity</topic><topic>Finite difference method</topic><topic>Fluid dynamics</topic><topic>Fluid flow</topic><topic>GPU</topic><topic>high order</topic><topic>Hydrodynamics</topic><topic>OpenSBLI</topic><topic>Resolution</topic><topic>Shock capturing</topic><topic>Spatial discrimination</topic><topic>Spatial resolution</topic><topic>Spectral methods</topic><topic>Statistical methods</topic><topic>Supersonic flow</topic><topic>TENO</topic><topic>Turbulence</topic><topic>Turbulent flow</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hamzehloo, Arash</creatorcontrib><creatorcontrib>Lusher, David J.</creatorcontrib><creatorcontrib>Laizet, Sylvain</creatorcontrib><creatorcontrib>Sandham, Neil D.</creatorcontrib><collection>Wiley-Blackwell Open Access Titles</collection><collection>CrossRef</collection><collection>Aqualine</collection><collection>Computer and Information Systems Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Water Resources Abstracts</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ASFA: Aquatic Sciences and Fisheries Abstracts</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Aquatic Science & Fisheries Abstracts (ASFA) 2: Ocean Technology, Policy & Non-Living Resources</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Aquatic Science & Fisheries Abstracts (ASFA) Professional</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>International journal for numerical methods in fluids</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hamzehloo, Arash</au><au>Lusher, David J.</au><au>Laizet, Sylvain</au><au>Sandham, Neil D.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>On the performance of WENO/TENO schemes to resolve turbulence in DNS/LES of high‐speed compressible flows</atitle><jtitle>International journal for numerical methods in fluids</jtitle><date>2021-01</date><risdate>2021</risdate><volume>93</volume><issue>1</issue><spage>176</spage><epage>196</epage><pages>176-196</pages><issn>0271-2091</issn><eissn>1097-0363</eissn><abstract>Summary
High‐speed compressible turbulent flows typically contain discontinuities and have been widely modeled using Weighted Essentially Non‐Oscillatory (WENO) schemes due to their high‐order accuracy and sharp shock capturing capability. However, such schemes may damp the small scales of turbulence and result in inaccurate solutions in the context of turbulence‐resolving simulations. In this connection, the recently developed Targeted Essentially Non‐Oscillatory (TENO) schemes, including adaptive variants, may offer significant improvements. The present study aims to quantify the potential of these new schemes for a fully turbulent supersonic flow. Specifically, DNS of a compressible turbulent channel flow with M = 1.5 and Reτ = 222 is conducted using OpenSBLI, a high‐order finite difference computational fluid dynamics framework. This flow configuration is chosen to decouple the effect of flow discontinuities and turbulence and focus on the capability of the aforementioned high‐order schemes to resolve turbulent structures. The effect of the spatial resolution in different directions and coarse grid implicit LES are also evaluated against the WALE LES model. The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. Although the most computationally expensive scheme, it is shown that this adaptive scheme can produce satisfactory results if used as an implicit LES model.
The TENO schemes are found to exhibit significant performance improvements over the WENO schemes in terms of the accuracy of the statistics and the resolution of the three‐dimensional vortical structures. The sixth‐order adaptive TENO scheme is found to produce comparable results to those obtained with nondissipative fourth‐ and sixth‐order central schemes and reference data obtained with spectral methods. The adaptive TENO scheme can produce satisfactory results if used as an implicit LES model.</abstract><cop>Hoboken, USA</cop><pub>John Wiley & Sons, Inc</pub><doi>10.1002/fld.4879</doi><tpages>22</tpages><orcidid>https://orcid.org/0000-0003-1470-4490</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Accuracy Channel flow code generation Compressible flow Computational fluid dynamics Computer applications Discontinuity Finite difference method Fluid dynamics Fluid flow GPU high order Hydrodynamics OpenSBLI Resolution Shock capturing Spatial discrimination Spatial resolution Spectral methods Statistical methods Supersonic flow TENO Turbulence Turbulent flow |
title | On the performance of WENO/TENO schemes to resolve turbulence in DNS/LES of high‐speed compressible flows |
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