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    Drag on an Oscillating Airfoil in a Fluctuating Free Stream

    Source: Journal of Fluids Engineering:;1979:;volume( 101 ):;issue: 003::page 391
    Author:
    S. B. R. Kottapalli
    ,
    G. Alvin Pierce
    DOI: 10.1115/1.3448985
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical study is presented regarding the unsteady skin friction drag of an oscillating airfoil exposed to a fluctuating free stream speed. Both laminar and turbulent conditions are covered in the analysis. The unsteady potential flow pressure and velocity distributions required for the subsequent boundary layer analysis are obtained by an approximate development. The time-dependent boundary layer is solved by a finite difference scheme. It was found that depending on the values of the phase difference between free stream fluctuations and airfoil oscillations, reduced frequency, and amplitude of free stream fluctuations, the drag can either lead or lag the free stream.
    keyword(s): Drag (Fluid dynamics) , Airfoils , Boundary layers , Fluctuations (Physics) , Skin friction (Fluid dynamics) , Oscillations , Pressure , Flow (Dynamics) AND Turbulence ,
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      Drag on an Oscillating Airfoil in a Fluctuating Free Stream

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    https://yetl.yabesh.ir/yetl1/handle/yetl/92299
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    contributor authorS. B. R. Kottapalli
    contributor authorG. Alvin Pierce
    date accessioned2017-05-08T23:07:01Z
    date available2017-05-08T23:07:01Z
    date copyrightSeptember, 1979
    date issued1979
    identifier issn0098-2202
    identifier otherJFEGA4-26948#391_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92299
    description abstractAn analytical study is presented regarding the unsteady skin friction drag of an oscillating airfoil exposed to a fluctuating free stream speed. Both laminar and turbulent conditions are covered in the analysis. The unsteady potential flow pressure and velocity distributions required for the subsequent boundary layer analysis are obtained by an approximate development. The time-dependent boundary layer is solved by a finite difference scheme. It was found that depending on the values of the phase difference between free stream fluctuations and airfoil oscillations, reduced frequency, and amplitude of free stream fluctuations, the drag can either lead or lag the free stream.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDrag on an Oscillating Airfoil in a Fluctuating Free Stream
    typeJournal Paper
    journal volume101
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448985
    journal fristpage391
    journal lastpage399
    identifier eissn1528-901X
    keywordsDrag (Fluid dynamics)
    keywordsAirfoils
    keywordsBoundary layers
    keywordsFluctuations (Physics)
    keywordsSkin friction (Fluid dynamics)
    keywordsOscillations
    keywordsPressure
    keywordsFlow (Dynamics) AND Turbulence
    treeJournal of Fluids Engineering:;1979:;volume( 101 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian