Thermal Dynamic Problems of Reinforced Composite CylindersSource: Journal of Applied Mechanics:;1990:;volume( 057 ):;issue: 004::page 941Author:Victor Birman
DOI: 10.1115/1.2897665Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Thermal dynamic problems of circular cylindrical composite shells reinforced in the axial and circumferential directions and subject to variations of temperature are considered. Nonlinear governing equations are formulated based on the extension of Donnell shell theory. These equations are used to determine the response of geometrically nonlinear and linear shells to a thermal loading represented by the Heaviside step function (thermal shock). The solution of the nonlinear problem obtained by the assumption that displacements are single-term functions of coordinates is discussed. The analysis of the linear problem illustrates different types of response to thermal shock. The condition of thermally-induced buckling of shells is formulated. Numerical analysis results in conclusions regarding the behavior of shells subject to thermal shock if the temperature is uniformly distributed throughout the shell and stiffeners.
keyword(s): Composite materials , Cylinders , Shells , Thermal shock , Temperature , Equations , Functions , Numerical analysis AND Buckling ,
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| contributor author | Victor Birman | |
| date accessioned | 2017-05-08T23:31:39Z | |
| date available | 2017-05-08T23:31:39Z | |
| date copyright | December, 1990 | |
| date issued | 1990 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26328#941_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/106353 | |
| description abstract | Thermal dynamic problems of circular cylindrical composite shells reinforced in the axial and circumferential directions and subject to variations of temperature are considered. Nonlinear governing equations are formulated based on the extension of Donnell shell theory. These equations are used to determine the response of geometrically nonlinear and linear shells to a thermal loading represented by the Heaviside step function (thermal shock). The solution of the nonlinear problem obtained by the assumption that displacements are single-term functions of coordinates is discussed. The analysis of the linear problem illustrates different types of response to thermal shock. The condition of thermally-induced buckling of shells is formulated. Numerical analysis results in conclusions regarding the behavior of shells subject to thermal shock if the temperature is uniformly distributed throughout the shell and stiffeners. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Thermal Dynamic Problems of Reinforced Composite Cylinders | |
| type | Journal Paper | |
| journal volume | 57 | |
| journal issue | 4 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.2897665 | |
| journal fristpage | 941 | |
| journal lastpage | 947 | |
| identifier eissn | 1528-9036 | |
| keywords | Composite materials | |
| keywords | Cylinders | |
| keywords | Shells | |
| keywords | Thermal shock | |
| keywords | Temperature | |
| keywords | Equations | |
| keywords | Functions | |
| keywords | Numerical analysis AND Buckling | |
| tree | Journal of Applied Mechanics:;1990:;volume( 057 ):;issue: 004 | |
| contenttype | Fulltext |