Bounds on the Maximum Thermoelastic Stress and Deflection in a Beam and PlateSource: Journal of Applied Mechanics:;1966:;volume( 033 ):;issue: 004::page 881Author:Bruno A. Boley
DOI: 10.1115/1.3625197Publisher: 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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| contributor author | Bruno A. Boley | |
| date accessioned | 2017-05-08T23:37:53Z | |
| date available | 2017-05-08T23:37:53Z | |
| date copyright | December, 1966 | |
| date issued | 1966 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-25839#881_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109934 | |
| description 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Bounds on the Maximum Thermoelastic Stress and Deflection in a Beam and Plate | |
| type | Journal Paper | |
| journal volume | 33 | |
| journal issue | 4 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3625197 | |
| journal fristpage | 881 | |
| journal lastpage | 887 | |
| identifier eissn | 1528-9036 | |
| keywords | Stress | |
| keywords | Deflection | |
| keywords | Shapes | |
| keywords | Simply supported beams | |
| keywords | Formulas | |
| keywords | Force | |
| keywords | Temperature | |
| keywords | Cross section (Physics) | |
| keywords | Thermal stresses AND Plates (structures) | |
| tree | Journal of Applied Mechanics:;1966:;volume( 033 ):;issue: 004 | |
| contenttype | Fulltext |