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    Comparison of Computational and Experimental Unsteady Cavitation on a Pitching Foil

    Source: Journal of Fluids Engineering:;1989:;volume( 111 ):;issue: 003::page 290
    Author:
    F. Stern
    DOI: 10.1115/1.3243643
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Comparisons are made between a nonlinear method for predicting unsteady sheet cavitation and available experimental data for a pitching foil for the purposes of verifying the calculations and to further analyze the flow. A dynamical approach is employed in which the form of the instantaneous cavity surface is modeled as a semiellipse. The cavity length (major axis), thickness (semiminor axis), and position are determined such that the nonlinear cavity-surface boundary conditions are satisfied approximately. The pressure on the instantaneous cavity surface is prescribed using an unsteady thick-foil potential-flow method based on Green’s second identity. The computational method yields best results in predicting the cavity dynamics, but underpredicts the cavity length. For fixed cavitation number, mean foil angle, and pitch amplitude, the cavity dynamics, such as maximum cavity size and cavity surface behavior, are shown to depend on the ratio of the cavity natural frequency for the foil fixed at the maximum pitch amplitude to the foil reduced frequency. For a certain value of this ratio, the cavitation response is shown to be a minimum. The experimental results confirm the computational trends up to the point that experimental data were obtained.
    keyword(s): Cavitation , Cavities , Flow (Dynamics) , Dynamics (Mechanics) , Pressure , Boundary-value problems , Thickness AND Computational methods ,
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      Comparison of Computational and Experimental Unsteady Cavitation on a Pitching Foil

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    http://yetl.yabesh.ir/yetl1/handle/yetl/105562
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    contributor authorF. Stern
    date accessioned2017-05-08T23:30:16Z
    date available2017-05-08T23:30:16Z
    date copyrightSeptember, 1989
    date issued1989
    identifier issn0098-2202
    identifier otherJFEGA4-27044#290_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105562
    description abstractComparisons are made between a nonlinear method for predicting unsteady sheet cavitation and available experimental data for a pitching foil for the purposes of verifying the calculations and to further analyze the flow. A dynamical approach is employed in which the form of the instantaneous cavity surface is modeled as a semiellipse. The cavity length (major axis), thickness (semiminor axis), and position are determined such that the nonlinear cavity-surface boundary conditions are satisfied approximately. The pressure on the instantaneous cavity surface is prescribed using an unsteady thick-foil potential-flow method based on Green’s second identity. The computational method yields best results in predicting the cavity dynamics, but underpredicts the cavity length. For fixed cavitation number, mean foil angle, and pitch amplitude, the cavity dynamics, such as maximum cavity size and cavity surface behavior, are shown to depend on the ratio of the cavity natural frequency for the foil fixed at the maximum pitch amplitude to the foil reduced frequency. For a certain value of this ratio, the cavitation response is shown to be a minimum. The experimental results confirm the computational trends up to the point that experimental data were obtained.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComparison of Computational and Experimental Unsteady Cavitation on a Pitching Foil
    typeJournal Paper
    journal volume111
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3243643
    journal fristpage290
    journal lastpage299
    identifier eissn1528-901X
    keywordsCavitation
    keywordsCavities
    keywordsFlow (Dynamics)
    keywordsDynamics (Mechanics)
    keywordsPressure
    keywordsBoundary-value problems
    keywordsThickness AND Computational methods
    treeJournal of Fluids Engineering:;1989:;volume( 111 ):;issue: 003
    contenttypeFulltext
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