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    A Methodology for Simulating Compressible Turbulent Flows

    Source: Journal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003::page 405
    Author:
    Hermann F. Fasel
    ,
    Dominic A. von Terzi
    ,
    Richard D. Sandberg
    DOI: 10.1115/1.2150231
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A flow simulation Methodology (FSM) is presented for computing the time-dependent behavior of complex compressible turbulent flows. The development of FSM was initiated in close collaboration with C. Speziale (then at Boston University). The objective of FSM is to provide the proper amount of turbulence modeling for the unresolved scales while directly computing the largest scales. The strategy is implemented by using state-of-the-art turbulence models (as developed for Reynolds averaged Navier-Stokes (RANS)) and scaling of the model terms with a “contribution function.” The contribution function is dependent on the local and instantaneous “physical” resolution in the computation. This physical resolution is determined during the actual simulation by comparing the size of the smallest relevant scales to the local grid size used in the computation. The contribution function is designed such that it provides no modeling if the computation is locally well resolved so that it approaches direct numerical simulations (DNS) in the fine-grid limit and such that it provides modeling of all scales in the coarse-grid limit and thus approaches a RANS calculation. In between these resolution limits, the contribution function adjusts the necessary modeling for the unresolved scales while the larger (resolved) scales are computed as in large eddy simulation (LES). However, FSM is distinctly different from LES in that it allows for a consistent transition between RANS, LES, and DNS within the same simulation depending on the local flow behavior and “physical” resolution. As a consequence, FSM should require considerably fewer grid points for a given calculation than would be necessary for a LES. This conjecture is substantiated by employing FSM to calculate the flow over a backward-facing step and a plane wake behind a bluff body, both at low Mach number, and supersonic axisymmetric wakes. These examples were chosen such that they expose, on the one hand, the inherent difficulties of simulating (physically) complex flows, and, on the other hand, demonstrate the potential of the FSM approach for simulations of turbulent compressible flows for complex geometries.
    keyword(s): Flow (Dynamics) , Turbulence , Wakes , Reynolds-averaged Navier–Stokes equations AND Equations ,
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      A Methodology for Simulating Compressible Turbulent Flows

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    https://yetl.yabesh.ir/yetl1/handle/yetl/133047
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    contributor authorHermann F. Fasel
    contributor authorDominic A. von Terzi
    contributor authorRichard D. Sandberg
    date accessioned2017-05-09T00:18:39Z
    date available2017-05-09T00:18:39Z
    date copyrightMay, 2006
    date issued2006
    identifier issn0021-8936
    identifier otherJAMCAV-26599#405_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133047
    description abstractA flow simulation Methodology (FSM) is presented for computing the time-dependent behavior of complex compressible turbulent flows. The development of FSM was initiated in close collaboration with C. Speziale (then at Boston University). The objective of FSM is to provide the proper amount of turbulence modeling for the unresolved scales while directly computing the largest scales. The strategy is implemented by using state-of-the-art turbulence models (as developed for Reynolds averaged Navier-Stokes (RANS)) and scaling of the model terms with a “contribution function.” The contribution function is dependent on the local and instantaneous “physical” resolution in the computation. This physical resolution is determined during the actual simulation by comparing the size of the smallest relevant scales to the local grid size used in the computation. The contribution function is designed such that it provides no modeling if the computation is locally well resolved so that it approaches direct numerical simulations (DNS) in the fine-grid limit and such that it provides modeling of all scales in the coarse-grid limit and thus approaches a RANS calculation. In between these resolution limits, the contribution function adjusts the necessary modeling for the unresolved scales while the larger (resolved) scales are computed as in large eddy simulation (LES). However, FSM is distinctly different from LES in that it allows for a consistent transition between RANS, LES, and DNS within the same simulation depending on the local flow behavior and “physical” resolution. As a consequence, FSM should require considerably fewer grid points for a given calculation than would be necessary for a LES. This conjecture is substantiated by employing FSM to calculate the flow over a backward-facing step and a plane wake behind a bluff body, both at low Mach number, and supersonic axisymmetric wakes. These examples were chosen such that they expose, on the one hand, the inherent difficulties of simulating (physically) complex flows, and, on the other hand, demonstrate the potential of the FSM approach for simulations of turbulent compressible flows for complex geometries.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Methodology for Simulating Compressible Turbulent Flows
    typeJournal Paper
    journal volume73
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2150231
    journal fristpage405
    journal lastpage412
    identifier eissn1528-9036
    keywordsFlow (Dynamics)
    keywordsTurbulence
    keywordsWakes
    keywordsReynolds-averaged Navier–Stokes equations AND Equations
    treeJournal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003
    contenttypeFulltext
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