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    Experimental Studies on a Nonlinear Hydroelastic Vibration of a Clamped Cylindrical Tank Partially Filled With Liquid

    Source: Journal of Pressure Vessel Technology:;1993:;volume( 115 ):;issue: 004::page 381
    Author:
    M. Chiba
    DOI: 10.1115/1.2929545
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental studies have been carried out on the nonlinear hydroelastic vibrations of a clamped circular cylindrical tank with a flexible wall and a rigid bottom. In the studies, two test cylinders, made of polyester, with radius R = 240 mm, thickness h = 0.254 mm, and length L = 480 and 160 mm (L/R = 2.0 and 2/3), respectively, were used. The tank is fully or partially filled with water having a free surface. The nonlinearity of the response of the flexible wall when the wall of the tank is harmonically excited by points was investigated, with varying liquid height. It was found that the degree of the nonlinearity depends on the vibration mode, i.e., a circumferential wave number and an axial wave number of the shell, on the length of the tank, as well as on the height of the liquid contained in it. The results obtained here were compared with the experimental results of a cantilevered tank, which was previously carried out. The influence of a thin film floating on the free surface upon the bulging-type responses, in which shell wall response is predominant, was also examined. On the free surface, sub-harmonic response with order 1/2 was observed when the amplitude of the shell wall became large.
    keyword(s): Vibration , Shells , Waves , Thickness , Water , Cylinders , Thin films AND Polyester fabrics ,
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      Experimental Studies on a Nonlinear Hydroelastic Vibration of a Clamped Cylindrical Tank Partially Filled With Liquid

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    http://yetl.yabesh.ir/yetl1/handle/yetl/112503
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    contributor authorM. Chiba
    date accessioned2017-05-08T23:42:18Z
    date available2017-05-08T23:42:18Z
    date copyrightNovember, 1993
    date issued1993
    identifier issn0094-9930
    identifier otherJPVTAS-28349#381_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112503
    description abstractExperimental studies have been carried out on the nonlinear hydroelastic vibrations of a clamped circular cylindrical tank with a flexible wall and a rigid bottom. In the studies, two test cylinders, made of polyester, with radius R = 240 mm, thickness h = 0.254 mm, and length L = 480 and 160 mm (L/R = 2.0 and 2/3), respectively, were used. The tank is fully or partially filled with water having a free surface. The nonlinearity of the response of the flexible wall when the wall of the tank is harmonically excited by points was investigated, with varying liquid height. It was found that the degree of the nonlinearity depends on the vibration mode, i.e., a circumferential wave number and an axial wave number of the shell, on the length of the tank, as well as on the height of the liquid contained in it. The results obtained here were compared with the experimental results of a cantilevered tank, which was previously carried out. The influence of a thin film floating on the free surface upon the bulging-type responses, in which shell wall response is predominant, was also examined. On the free surface, sub-harmonic response with order 1/2 was observed when the amplitude of the shell wall became large.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Studies on a Nonlinear Hydroelastic Vibration of a Clamped Cylindrical Tank Partially Filled With Liquid
    typeJournal Paper
    journal volume115
    journal issue4
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.2929545
    journal fristpage381
    journal lastpage388
    identifier eissn1528-8978
    keywordsVibration
    keywordsShells
    keywordsWaves
    keywordsThickness
    keywordsWater
    keywordsCylinders
    keywordsThin films AND Polyester fabrics
    treeJournal of Pressure Vessel Technology:;1993:;volume( 115 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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