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    Computation of Unsteady Viscous Marine-Propulsor Blade Flows—Part 1: Validation and Analysis

    Source: Journal of Fluids Engineering:;1997:;volume( 119 ):;issue: 001::page 145
    Author:
    E. G. Paterson
    ,
    F. Stern
    DOI: 10.1115/1.2819100
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this two-part paper, time-accurate solutions of the Reynolds-averaged Navier-Stokes equations are presented, which address through model problems, the response of turbulent propeller-blade boundary layers, and wakes to external-flow traveling waves. In Part 1, the Massachusetts Institute of Technology flapping-foil experiment is simulated and the results validated through comparisons with data. The physics of unsteady blade flows are shown to be complex with analogy to Stokes layers and are explicated through visualization and Fourier analysis. It is shown that convection induced steady/unsteady interaction causes deformation of the external-flow waves and is responsible for the upstream- and downstream-traveling pressure-gradient waves over the foil and in the wake, respectively. The nature of the unsteady displacement thickness suggests viscous-inviscid interaction as the mechanism for the response. In Part 2, a parametric study is undertaken to quantify the effects of frequency, foil geometry, and waveform.
    keyword(s): Blades , Computation , Flow (Dynamics) , Waves , Wakes , Travel , Mechanisms , Deformation , Turbulence , Navier-Stokes equations , Boundary layers , Convection , Visualization , Displacement , Fourier analysis , Geometry , Pressure gradient , Propellers , Thickness AND Physics ,
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      Computation of Unsteady Viscous Marine-Propulsor Blade Flows—Part 1: Validation and Analysis

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    http://yetl.yabesh.ir/yetl1/handle/yetl/118981
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    contributor authorE. G. Paterson
    contributor authorF. Stern
    date accessioned2017-05-08T23:54:00Z
    date available2017-05-08T23:54:00Z
    date copyrightMarch, 1997
    date issued1997
    identifier issn0098-2202
    identifier otherJFEGA4-27114#145_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118981
    description abstractIn this two-part paper, time-accurate solutions of the Reynolds-averaged Navier-Stokes equations are presented, which address through model problems, the response of turbulent propeller-blade boundary layers, and wakes to external-flow traveling waves. In Part 1, the Massachusetts Institute of Technology flapping-foil experiment is simulated and the results validated through comparisons with data. The physics of unsteady blade flows are shown to be complex with analogy to Stokes layers and are explicated through visualization and Fourier analysis. It is shown that convection induced steady/unsteady interaction causes deformation of the external-flow waves and is responsible for the upstream- and downstream-traveling pressure-gradient waves over the foil and in the wake, respectively. The nature of the unsteady displacement thickness suggests viscous-inviscid interaction as the mechanism for the response. In Part 2, a parametric study is undertaken to quantify the effects of frequency, foil geometry, and waveform.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComputation of Unsteady Viscous Marine-Propulsor Blade Flows—Part 1: Validation and Analysis
    typeJournal Paper
    journal volume119
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2819100
    journal fristpage145
    journal lastpage154
    identifier eissn1528-901X
    keywordsBlades
    keywordsComputation
    keywordsFlow (Dynamics)
    keywordsWaves
    keywordsWakes
    keywordsTravel
    keywordsMechanisms
    keywordsDeformation
    keywordsTurbulence
    keywordsNavier-Stokes equations
    keywordsBoundary layers
    keywordsConvection
    keywordsVisualization
    keywordsDisplacement
    keywordsFourier analysis
    keywordsGeometry
    keywordsPressure gradient
    keywordsPropellers
    keywordsThickness AND Physics
    treeJournal of Fluids Engineering:;1997:;volume( 119 ):;issue: 001
    contenttypeFulltext
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