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    Analysis of Unsteady Laminar Boundary Layer Flow by an Integral Method

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 002::page 237
    Author:
    R. W. Miller
    ,
    L. S. Han
    DOI: 10.1115/1.3447001
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate integral method of analysis is developed for unsteady laminar boundary layer flows. The case of a flat plate in a free stream with small harmonic velocity oscillations about a steady mean is used to formulate the method. Results are compared with the available experimental data. The essence of the method is to: First obtain asymptotic solutions for limiting cases of the flow under consideration. Then, assume velocity profiles with sufficient generality to include the asymptotic solutions. The profile form functions are determined by applying integral relations (velocity weighted averages of the momentum equation) and compatibility conditions (normal derivatives of the momentum equation evaluated at the boundary). As an example of the method, the second-order mean flow correction is determined for oscillating flow over a flat plate.
    keyword(s): Flow (Dynamics) , Boundary layers , Equations , Flat plates , Momentum , Oscillations AND Functions ,
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      Analysis of Unsteady Laminar Boundary Layer Flow by an Integral Method

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/163915
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    • Journal of Fluids Engineering

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    contributor authorR. W. Miller
    contributor authorL. S. Han
    date accessioned2017-05-09T01:36:37Z
    date available2017-05-09T01:36:37Z
    date copyrightJune, 1973
    date issued1973
    identifier issn0098-2202
    identifier otherJFEGA4-26845#237_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163915
    description abstractAn approximate integral method of analysis is developed for unsteady laminar boundary layer flows. The case of a flat plate in a free stream with small harmonic velocity oscillations about a steady mean is used to formulate the method. Results are compared with the available experimental data. The essence of the method is to: First obtain asymptotic solutions for limiting cases of the flow under consideration. Then, assume velocity profiles with sufficient generality to include the asymptotic solutions. The profile form functions are determined by applying integral relations (velocity weighted averages of the momentum equation) and compatibility conditions (normal derivatives of the momentum equation evaluated at the boundary). As an example of the method, the second-order mean flow correction is determined for oscillating flow over a flat plate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Unsteady Laminar Boundary Layer Flow by an Integral Method
    typeJournal Paper
    journal volume95
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3447001
    journal fristpage237
    journal lastpage247
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsBoundary layers
    keywordsEquations
    keywordsFlat plates
    keywordsMomentum
    keywordsOscillations AND Functions
    treeJournal of Fluids Engineering:;1973:;volume( 095 ):;issue: 002
    contenttypeFulltext
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