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    Elastic Response of a Thin Conical Shell to an Oblique Impact

    Source: Journal of Applied Mechanics:;1973:;volume( 040 ):;issue: 004::page 1017
    Author:
    B. Albrecht
    ,
    W. E. Baker
    ,
    M. Valathur
    DOI: 10.1115/1.3423118
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Strain waves in a truncated conical shell generated by oblique impact of the small end of the shell are discussed. The analysis is based on the general first-order linear shell theory of Sanders with all pertinent variables expanded into Fourier series in circumferential direction, resulting in decoupled sets of ordinary differential equations. Finite-difference approximations to these differential equations are then solved by matrix techniques. Theoretical values compare well with experimental results for the angle of oblicity β = 0, 5, 10, and 15 deg, the range of the experimental work.
    keyword(s): Shells , Differential equations , Approximation , Fourier series AND Waves ,
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      Elastic Response of a Thin Conical Shell to an Oblique Impact

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    http://yetl.yabesh.ir/yetl1/handle/yetl/163356
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    contributor authorB. Albrecht
    contributor authorW. E. Baker
    contributor authorM. Valathur
    date accessioned2017-05-09T01:35:41Z
    date available2017-05-09T01:35:41Z
    date copyrightDecember, 1973
    date issued1973
    identifier issn0021-8936
    identifier otherJAMCAV-25994#1017_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163356
    description abstractStrain waves in a truncated conical shell generated by oblique impact of the small end of the shell are discussed. The analysis is based on the general first-order linear shell theory of Sanders with all pertinent variables expanded into Fourier series in circumferential direction, resulting in decoupled sets of ordinary differential equations. Finite-difference approximations to these differential equations are then solved by matrix techniques. Theoretical values compare well with experimental results for the angle of oblicity β = 0, 5, 10, and 15 deg, the range of the experimental work.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleElastic Response of a Thin Conical Shell to an Oblique Impact
    typeJournal Paper
    journal volume40
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3423118
    journal fristpage1017
    journal lastpage1022
    identifier eissn1528-9036
    keywordsShells
    keywordsDifferential equations
    keywordsApproximation
    keywordsFourier series AND Waves
    treeJournal of Applied Mechanics:;1973:;volume( 040 ):;issue: 004
    contenttypeFulltext
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