Thermoelastic buckling of thin cylindrical shells based on improved stability equations

被引:48
作者
Eslami, MR
Ziaii, AR
Ghorbanpour, A
机构
[1] Department of Mechanical Engineering, Amirkabir Uniuersity of Technology, Tehran
关键词
D O I
10.1080/01495739608946177
中图分类号
O414.1 [热力学];
学科分类号
摘要
The nonlinear strain-displacement relations in general cylindrical coordinates are simplified by Sander's assumptions for the cylindrical shells and substituted into the total potential energy function for thermoelastic loading. The Euler equations are then applied to the functional of energy, and the general thermoelastic equations of nonlinear shell theory are obtained and compared with the Donnel equations. An improvement is observed in the resulting equations as no length limitations are imposed on a thin cylindrical shell. The stability equations are then derived through the second variation of potential energy, and the same improvements are extended to the resulting thermoelastic stability equations. Based on the improved equilibrium and stability equations, the magnitude of thermoelastic buckling of thin cylindrical shells under different thermal loadings is obtained. The results are extended to short and long thin cylindrical shells.
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收藏
页码:299 / 315
页数:17
相关论文
共 17 条
[1]  
[Anonymous], TND1510 NASA
[2]  
[Anonymous], 1973, STRESSES SHELLS, DOI DOI 10.1007/978-3-642-88291-3
[3]  
[Anonymous], 1976, BEAMS PLATES SHELLS
[4]  
Brush D., 1975, Buckling of Bars, Plates and Shells, DOI DOI 10.1115/1.3423755
[6]  
CHANG LK, 1970, P AIAA ASME 11 STRUC, P260
[7]  
DONNEL LH, 1958, J APPL MECH, V28, P305
[8]  
Donnell L.H., 1956, J APPL MECH, V23, P569
[9]  
DONNELL LH, 1950, J APPL MECH-T ASME, V17, P73
[10]  
ESLAMI MR, 1992, P ASME ESDA C, V1, P401