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    Stress Analysis for a Nonlinear Viscoelastic Cylinder With Ablating Inner Surface

    Source: Journal of Applied Mechanics:;1970:;volume( 037 ):;issue: 001::page 44
    Author:
    E. C. Ting
    DOI: 10.1115/1.3408487
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate constitutive equation for nonlinear viscoelastic incompressible materials under small finite deformation and for short time ranges has been derived by Huang and Lee [1]. The resulting equation is applied to solve the problem of a pressurized viscoelastic hollow cylinder bonded to an elastic easing. This problem is of notable technical interest in solid propellant stress analysis, since it is a close model to represent a cylindrical propellant grain in a solid fuel rocket under firing condition. The method used by Huang and Lee is appropriate for numerical calculations when the boundaries of the cylinder are nonablating. To consider one step closer to the real situation, the inner surface is often assumed to be ablating and hence time-dependent. It is then the purpose of the present paper to extend the analysis to a cylinder with moving inner surface.
    keyword(s): Stress analysis (Engineering) , Cylinders , Equations , Propellants , Rockets , Deformation , Fuels AND Firing (materials) ,
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      Stress Analysis for a Nonlinear Viscoelastic Cylinder With Ablating Inner Surface

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    https://yetl.yabesh.ir/yetl1/handle/yetl/141545
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    contributor authorE. C. Ting
    date accessioned2017-05-09T00:34:41Z
    date available2017-05-09T00:34:41Z
    date copyrightMarch, 1970
    date issued1970
    identifier issn0021-8936
    identifier otherJAMCAV-25906#44_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/141545
    description abstractAn approximate constitutive equation for nonlinear viscoelastic incompressible materials under small finite deformation and for short time ranges has been derived by Huang and Lee [1]. The resulting equation is applied to solve the problem of a pressurized viscoelastic hollow cylinder bonded to an elastic easing. This problem is of notable technical interest in solid propellant stress analysis, since it is a close model to represent a cylindrical propellant grain in a solid fuel rocket under firing condition. The method used by Huang and Lee is appropriate for numerical calculations when the boundaries of the cylinder are nonablating. To consider one step closer to the real situation, the inner surface is often assumed to be ablating and hence time-dependent. It is then the purpose of the present paper to extend the analysis to a cylinder with moving inner surface.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStress Analysis for a Nonlinear Viscoelastic Cylinder With Ablating Inner Surface
    typeJournal Paper
    journal volume37
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3408487
    journal fristpage44
    journal lastpage47
    identifier eissn1528-9036
    keywordsStress analysis (Engineering)
    keywordsCylinders
    keywordsEquations
    keywordsPropellants
    keywordsRockets
    keywordsDeformation
    keywordsFuels AND Firing (materials)
    treeJournal of Applied Mechanics:;1970:;volume( 037 ):;issue: 001
    contenttypeFulltext
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