POSTBUCKLING OF INFINITE LENGTH CYLINDRICAL PANELS UNDER COMBINED THERMAL AND PRESSURE LOADING

被引:10
作者
WELLER, T
PATLASHENKO, I
机构
[1] Faculty of Aerospace Engineering, Technion-Israel Institute of Technology, Haifa
关键词
D O I
10.1016/0020-7683(93)90195-D
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An analysis for the pre- and postbuckling behavior of infinite length panels, stiffened and unstiffened, including transverse shear and temperature dependent elastic moduli and thermal expansion coefficients, is proposed. The analysis involves the solution of a system of nonlinear differential equations by means of a relatively new spline-collocation method. Results, yielded by the present study and describing the response of lightly to moderately stringer-stiffened panels and unstiffened ones, subjected to heating and pressure loading, are presented. It is shown that neglect of transverse shear and temperature effects may lead to erroneous results and conclusions.
引用
收藏
页码:1649 / 1662
页数:14
相关论文
共 22 条
[1]  
ANDREEV LV, 1988, STABILITY NONSYMMETR
[2]  
[Anonymous], 1981, INTRO NUMERICAL METH
[3]  
Baruch M, 1963, J MECH ENG SCI, V5, P23, DOI DOI 10.1243/JMES_JOUR_1963_005_005_02
[4]  
GRIGORENKO JM, 1977, DOPOV AKAD NAUK A, P417
[5]  
JACKSON LR, 1987, AERO AM OCT, P24
[6]  
KEENE FW, 1990, J THERM STRESSES, V13, pU341
[7]  
KHOROSHUN LP, 1988, PRIKL MEKH, V24, P38
[8]  
KHOROSHUN LP, 1988, PRIKL MEKH, V24, P56
[9]  
KRYSKO VA, 1984, PRIKL MEKH, V20, P44
[10]   THE EFFECT OF SHEAR DEFORMATION ON POSTBUCKLING BEHAVIOR OF LAMINATED BEAMS [J].
SHEINMAN, I ;
ADAN, M .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1987, 54 (03) :558-562