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    A Kriging Approach for CFD/Wind-Tunnel Data Comparison

    Source: Journal of Fluids Engineering:;2006:;volume( 128 ):;issue: 004::page 847
    Author:
    J.-C. Jouhaud
    ,
    P. Sagaut
    ,
    B. Labeyrie
    DOI: 10.1115/1.2201642
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A Kriging-based method for the parametrization of the response surface spanned by uncertain parameters in computational fluid dynamics is proposed. A multiresolution approach in the sampling space is used to improve the accuracy of the method. It is illustrated considering the problem of the computation of the corrections needed to recover equivalent free-flight conditions from wind-tunnel experiments. Using the surface response approach, optimal corrected values of the freestream Mach number and the angle of attack for the compressible turbulent flow around the RAE 2822 wing are computed. The use of the response surface to gain an insight into the sensitivity of the results with respect to other parameter is also assessed.
    keyword(s): Mach number , Turbulence , Computational fluid dynamics , Equations , Response surface methodology , Wind tunnels , Flow (Dynamics) , Engineering simulation , Interpolation AND Sampling (Acoustical engineering) ,
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      A Kriging Approach for CFD/Wind-Tunnel Data Comparison

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/133921
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    • Journal of Fluids Engineering

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    contributor authorJ.-C. Jouhaud
    contributor authorP. Sagaut
    contributor authorB. Labeyrie
    date accessioned2017-05-09T00:20:18Z
    date available2017-05-09T00:20:18Z
    date copyrightJuly, 2006
    date issued2006
    identifier issn0098-2202
    identifier otherJFEGA4-27219#847_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133921
    description abstractA Kriging-based method for the parametrization of the response surface spanned by uncertain parameters in computational fluid dynamics is proposed. A multiresolution approach in the sampling space is used to improve the accuracy of the method. It is illustrated considering the problem of the computation of the corrections needed to recover equivalent free-flight conditions from wind-tunnel experiments. Using the surface response approach, optimal corrected values of the freestream Mach number and the angle of attack for the compressible turbulent flow around the RAE 2822 wing are computed. The use of the response surface to gain an insight into the sensitivity of the results with respect to other parameter is also assessed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Kriging Approach for CFD/Wind-Tunnel Data Comparison
    typeJournal Paper
    journal volume128
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2201642
    journal fristpage847
    journal lastpage855
    identifier eissn1528-901X
    keywordsMach number
    keywordsTurbulence
    keywordsComputational fluid dynamics
    keywordsEquations
    keywordsResponse surface methodology
    keywordsWind tunnels
    keywordsFlow (Dynamics)
    keywordsEngineering simulation
    keywordsInterpolation AND Sampling (Acoustical engineering)
    treeJournal of Fluids Engineering:;2006:;volume( 128 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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