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    Comparison of RANS and Detached Eddy Simulation Results to Wind Tunnel Data for the Surface Pressures Upon a Class 43 High Speed Train

    Source: Journal of Fluids Engineering:;2015:;volume( 137 ):;issue: 004::page 41108
    Author:
    Morden, Justin A.
    ,
    Hemida, Hassan
    ,
    Baker, Chris. J.
    DOI: 10.1115/1.4029261
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Currently, there are three different methodologies for evaluating the aerodynamics of trains; fullscale measurements, physical modeling using windtunnel, and moving train rigs and numerical modeling using computational fluid dynamics (CFD). Moreover, different approaches and turbulence modeling are normally used within the CFD framework. The work in this paper investigates the consistency of two of these methodologies; the windtunnel and the CFD by comparing the measured surface pressure with the computed CFD values. The CFD is based on ReynoldsAveraged Navier–Stokes (RANS) turbulence models (five models were used; the Spalart–Allmaras (S–A), kخµ, kخµ renormalization group (RNG), realizable kخµ, and shear stress transport (SST) kد‰) and two detached eddy simulation (DES) approaches; the standard DES and delayed detached eddy simulation (DDES). This work was carried out as part of a larger project to determine whether the current methods of CFD, model scale and fullscale testing provide consistent results and are able to achieve agreement with each other when used in the measurement of train aerodynamic phenomena. Similar to the windtunnel, the CFD approaches were applied to external aerodynamic flow around a 1/25th scale class 43 highspeed tunnel (HST) model. Comparison between the CFD results and windtunnel data were conducted using coefficients for surface pressure, measured at the windtunnel by pressure taps fitted over the surface of the train in loops. Four different meshes where tested with both the RANS SST kد‰ and DDES approaches to form a mesh sensitivity study. The four meshes featured 18, 24, 34, and 52 أ— 106 cells. A mesh of 34 أ— 106 cells was found to provide the best balance between accuracy and computational cost. Comparison of the results showed that the DES based approaches; in particular, the DDES approach was best able to replicate the windtunnel results within the margin of uncertainty.
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      Comparison of RANS and Detached Eddy Simulation Results to Wind Tunnel Data for the Surface Pressures Upon a Class 43 High Speed Train

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    contributor authorMorden, Justin A.
    contributor authorHemida, Hassan
    contributor authorBaker, Chris. J.
    date accessioned2017-05-09T01:18:52Z
    date available2017-05-09T01:18:52Z
    date issued2015
    identifier issn0098-2202
    identifier otherfe_137_04_041108.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158227
    description abstractCurrently, there are three different methodologies for evaluating the aerodynamics of trains; fullscale measurements, physical modeling using windtunnel, and moving train rigs and numerical modeling using computational fluid dynamics (CFD). Moreover, different approaches and turbulence modeling are normally used within the CFD framework. The work in this paper investigates the consistency of two of these methodologies; the windtunnel and the CFD by comparing the measured surface pressure with the computed CFD values. The CFD is based on ReynoldsAveraged Navier–Stokes (RANS) turbulence models (five models were used; the Spalart–Allmaras (S–A), kخµ, kخµ renormalization group (RNG), realizable kخµ, and shear stress transport (SST) kد‰) and two detached eddy simulation (DES) approaches; the standard DES and delayed detached eddy simulation (DDES). This work was carried out as part of a larger project to determine whether the current methods of CFD, model scale and fullscale testing provide consistent results and are able to achieve agreement with each other when used in the measurement of train aerodynamic phenomena. Similar to the windtunnel, the CFD approaches were applied to external aerodynamic flow around a 1/25th scale class 43 highspeed tunnel (HST) model. Comparison between the CFD results and windtunnel data were conducted using coefficients for surface pressure, measured at the windtunnel by pressure taps fitted over the surface of the train in loops. Four different meshes where tested with both the RANS SST kد‰ and DDES approaches to form a mesh sensitivity study. The four meshes featured 18, 24, 34, and 52 أ— 106 cells. A mesh of 34 أ— 106 cells was found to provide the best balance between accuracy and computational cost. Comparison of the results showed that the DES based approaches; in particular, the DDES approach was best able to replicate the windtunnel results within the margin of uncertainty.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComparison of RANS and Detached Eddy Simulation Results to Wind Tunnel Data for the Surface Pressures Upon a Class 43 High Speed Train
    typeJournal Paper
    journal volume137
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4029261
    journal fristpage41108
    journal lastpage41108
    identifier eissn1528-901X
    treeJournal of Fluids Engineering:;2015:;volume( 137 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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