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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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