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    Free Vibration of Continuous Skin-Stringer Panels

    Source: Journal of Applied Mechanics:;1960:;volume( 027 ):;issue: 004::page 669
    Author:
    Y. K. Lin
    DOI: 10.1115/1.3644080
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The determination of the natural frequencies and normal modes of vibration for continuous panels, representing more or less typical fuselage skin-panel construction for modern airplanes, is discussed in this paper. The time-dependent boundary conditions at the supporting stringers are considered. A numerical example is presented, and analytical results for a particular structural configuration agree favorably with available experimental measurements.
    keyword(s): Free vibrations , Skin , Frequency , Measurement , Construction , Vibration , Aircraft AND Boundary-value problems ,
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      Free Vibration of Continuous Skin-Stringer Panels

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    http://yetl.yabesh.ir/yetl1/handle/yetl/105833
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    contributor authorY. K. Lin
    date accessioned2017-05-08T23:30:45Z
    date available2017-05-08T23:30:45Z
    date copyrightDecember, 1960
    date issued1960
    identifier issn0021-8936
    identifier otherJAMCAV-25565#669_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105833
    description abstractThe determination of the natural frequencies and normal modes of vibration for continuous panels, representing more or less typical fuselage skin-panel construction for modern airplanes, is discussed in this paper. The time-dependent boundary conditions at the supporting stringers are considered. A numerical example is presented, and analytical results for a particular structural configuration agree favorably with available experimental measurements.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFree Vibration of Continuous Skin-Stringer Panels
    typeJournal Paper
    journal volume27
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3644080
    journal fristpage669
    journal lastpage676
    identifier eissn1528-9036
    keywordsFree vibrations
    keywordsSkin
    keywordsFrequency
    keywordsMeasurement
    keywordsConstruction
    keywordsVibration
    keywordsAircraft AND Boundary-value problems
    treeJournal of Applied Mechanics:;1960:;volume( 027 ):;issue: 004
    contenttypeFulltext
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