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    Bounds on the Maximum Thermoelastic Stress and Deflection in a Beam and Plate

    Source: Journal of Applied Mechanics:;1966:;volume( 033 ):;issue: 004::page 881
    Author:
    Bruno A. Boley
    DOI: 10.1115/1.3625197
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is shown in this paper that the thermal stress in a beam or plate cannot exceed the value kαEΔT, where ΔT is the maximum instantaneous temperature excursion in a cross section, and k is a coefficient dependent on the shape of the cross section. A simple general formula for k is found, and results for several special cases of practical interest are given. For rectangular beams (suitably oriented) and for plates, for example, k = 4/3. For any section, k = 1 if the thermal moment is zero; simplifications also occur if the thermal force is zero. The corresponding results for beam deflections are also carried out: The maximum deflection cannot exceed the value kδ kδ ′ αLΔT, where kδ and kδ ′ are coefficients depending respectively on the cross-sectional shape and on the end conditions. For example, for rectangular cross sections, kδ = 3/4; and for a simply supported beam, kδ ′ = 1/8.
    keyword(s): Stress , Deflection , Shapes , Simply supported beams , Formulas , Force , Temperature , Cross section (Physics) , Thermal stresses AND Plates (structures) ,
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      Bounds on the Maximum Thermoelastic Stress and Deflection in a Beam and Plate

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    http://yetl.yabesh.ir/yetl1/handle/yetl/109934
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    contributor authorBruno A. Boley
    date accessioned2017-05-08T23:37:53Z
    date available2017-05-08T23:37:53Z
    date copyrightDecember, 1966
    date issued1966
    identifier issn0021-8936
    identifier otherJAMCAV-25839#881_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109934
    description abstractIt is shown in this paper that the thermal stress in a beam or plate cannot exceed the value kαEΔT, where ΔT is the maximum instantaneous temperature excursion in a cross section, and k is a coefficient dependent on the shape of the cross section. A simple general formula for k is found, and results for several special cases of practical interest are given. For rectangular beams (suitably oriented) and for plates, for example, k = 4/3. For any section, k = 1 if the thermal moment is zero; simplifications also occur if the thermal force is zero. The corresponding results for beam deflections are also carried out: The maximum deflection cannot exceed the value kδ kδ ′ αLΔT, where kδ and kδ ′ are coefficients depending respectively on the cross-sectional shape and on the end conditions. For example, for rectangular cross sections, kδ = 3/4; and for a simply supported beam, kδ ′ = 1/8.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBounds on the Maximum Thermoelastic Stress and Deflection in a Beam and Plate
    typeJournal Paper
    journal volume33
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3625197
    journal fristpage881
    journal lastpage887
    identifier eissn1528-9036
    keywordsStress
    keywordsDeflection
    keywordsShapes
    keywordsSimply supported beams
    keywordsFormulas
    keywordsForce
    keywordsTemperature
    keywordsCross section (Physics)
    keywordsThermal stresses AND Plates (structures)
    treeJournal of Applied Mechanics:;1966:;volume( 033 ):;issue: 004
    contenttypeFulltext
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