Variational Equation of Motion for Coupled Flexure and Torsion of Bars of Thin-Walled Open Section Including Thermal EffectSource: Journal of Applied Mechanics:;1971:;volume( 038 ):;issue: 002::page 502Author:Yi-Yuan Yu
DOI: 10.1115/1.3408803Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Literature on flexure and torsion of bars of thin-walled open section is reviewed. The use of the variational equation of motion in solving problems of structural dynamics is further advocated. The variational equation of motion, together with the associated stress-displacement relations, is then derived for coupled flexure and torsion of the open section. Thermal effect is included, leading to a thermal twisting moment in addition to the usual thermal bending moments. For the special case of an open section with one axis of symmetry and with symmetrical heat input, only flexure is shown to be thermally inducible. The general result then reduces to the simple variational equation of flexural motion used in a separate study of the thermal flutter of a spacecraft boom.
keyword(s): Temperature effects , Bending (Stress) , Torsion , Equations of motion , Structural dynamics , Flutter (Aerodynamics) , Displacement , Equations , Space vehicles , Heat , Motion , Symmetry (Physics) AND Stress ,
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| contributor author | Yi-Yuan Yu | |
| date accessioned | 2017-05-09T00:51:21Z | |
| date available | 2017-05-09T00:51:21Z | |
| date copyright | June, 1971 | |
| date issued | 1971 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-25939#502_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/149144 | |
| description abstract | Literature on flexure and torsion of bars of thin-walled open section is reviewed. The use of the variational equation of motion in solving problems of structural dynamics is further advocated. The variational equation of motion, together with the associated stress-displacement relations, is then derived for coupled flexure and torsion of the open section. Thermal effect is included, leading to a thermal twisting moment in addition to the usual thermal bending moments. For the special case of an open section with one axis of symmetry and with symmetrical heat input, only flexure is shown to be thermally inducible. The general result then reduces to the simple variational equation of flexural motion used in a separate study of the thermal flutter of a spacecraft boom. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Variational Equation of Motion for Coupled Flexure and Torsion of Bars of Thin-Walled Open Section Including Thermal Effect | |
| type | Journal Paper | |
| journal volume | 38 | |
| journal issue | 2 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3408803 | |
| journal fristpage | 502 | |
| journal lastpage | 506 | |
| identifier eissn | 1528-9036 | |
| keywords | Temperature effects | |
| keywords | Bending (Stress) | |
| keywords | Torsion | |
| keywords | Equations of motion | |
| keywords | Structural dynamics | |
| keywords | Flutter (Aerodynamics) | |
| keywords | Displacement | |
| keywords | Equations | |
| keywords | Space vehicles | |
| keywords | Heat | |
| keywords | Motion | |
| keywords | Symmetry (Physics) AND Stress | |
| tree | Journal of Applied Mechanics:;1971:;volume( 038 ):;issue: 002 | |
| contenttype | Fulltext |