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    Reexamination of Unsteady Fluid Dynamic Forces on a Two-Dimensional Finite Plate at Small Mach Numbers

    Source: Journal of Applied Mechanics:;1980:;volume( 047 ):;issue: 004::page 720
    Author:
    Y. Matsuzaki
    ,
    T. Ueda
    DOI: 10.1115/1.3153780
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The Fourier transform theory is applied to the analytical determination of the disturbance velocity potential and pressure acting on a two-dimensional plate, in order to reexamine those of previous analyses by other investigators. Simplified expressions of the generalized forces are presented for incompressible and nearly incompressible flows. As the Mach number tends to zero, the virtual mass induced by an oscillating fluid becomes infinitely large for a natural mode symmetric with respect to the midchord point. It is recommended to take into account a symmetric mode which changes no fluid volume contained in a control surface, when a coupled flutter oscillation at very low Mach numbers is analyzed. Incorrectness in the generalized forces of the previous analyses is pointed out by comparing with the present analysis.
    keyword(s): Mach number , Fluid-dynamic forces , Fluids , Force , Pressure , Flow (Dynamics) , Flutter (Aerodynamics) , Fourier transforms AND Oscillations ,
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      Reexamination of Unsteady Fluid Dynamic Forces on a Two-Dimensional Finite Plate at Small Mach Numbers

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    http://yetl.yabesh.ir/yetl1/handle/yetl/92740
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    contributor authorY. Matsuzaki
    contributor authorT. Ueda
    date accessioned2017-05-08T23:07:45Z
    date available2017-05-08T23:07:45Z
    date copyrightDecember, 1980
    date issued1980
    identifier issn0021-8936
    identifier otherJAMCAV-26159#720_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92740
    description abstractThe Fourier transform theory is applied to the analytical determination of the disturbance velocity potential and pressure acting on a two-dimensional plate, in order to reexamine those of previous analyses by other investigators. Simplified expressions of the generalized forces are presented for incompressible and nearly incompressible flows. As the Mach number tends to zero, the virtual mass induced by an oscillating fluid becomes infinitely large for a natural mode symmetric with respect to the midchord point. It is recommended to take into account a symmetric mode which changes no fluid volume contained in a control surface, when a coupled flutter oscillation at very low Mach numbers is analyzed. Incorrectness in the generalized forces of the previous analyses is pointed out by comparing with the present analysis.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleReexamination of Unsteady Fluid Dynamic Forces on a Two-Dimensional Finite Plate at Small Mach Numbers
    typeJournal Paper
    journal volume47
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3153780
    journal fristpage720
    journal lastpage724
    identifier eissn1528-9036
    keywordsMach number
    keywordsFluid-dynamic forces
    keywordsFluids
    keywordsForce
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsFlutter (Aerodynamics)
    keywordsFourier transforms AND Oscillations
    treeJournal of Applied Mechanics:;1980:;volume( 047 ):;issue: 004
    contenttypeFulltext
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