Response of elliptical composite cylinders to internal pressure loading

被引:10
作者
Meyers, CA
Hyer, MW
机构
[1] VIRGINIA POLYTECH INST & STATE UNIV,DEPT ENGN SCI & MECH,BLACKSBURG,VA 24061
[2] MAT SCI CORP,FT WASHINGTON,PA
来源
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES | 1997年 / 4卷 / 04期
关键词
D O I
10.1080/10759419708945887
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The results from semianalytical predictions and experiments are used to study the response of composite cylinders with elliptical cross sections loaded with internal pressure, The results for ellipses are contrasted to the case of circular cylinders, The semianalytical approach is based on the methods of Marguerre, Rayleigh-Ritz, and Kantorovich, the radius of curvature and the displacements being approximated by expansions in harmonic series in the circumferential are-length coordinate, and the coefficients of the displacement series being unknown functions of x that are solved for using the finite-difference method, The experiments are described and results for a circular and an elliptical quasi-isotropic cylinder loaded to I atm internal pressure are compared with predictions. Correlations between the predictions and the experiments are, in general, quite good.
引用
收藏
页码:317 / 343
页数:27
相关论文
共 26 条
[1]  
Albus J, 1996, Z FLUGWISS WELTRAUM, V20, P117
[2]  
[Anonymous], 1986, SHELL THEORY GEN MET
[3]  
ARBOCZ J, 1981, N8217537 NASA
[4]  
Dym C. L., 1990, Introduction To the Theory of Shells
[5]  
DYM CL, 1985, ENERGY FINITE ELEMEN, P71
[6]  
Flugge W, 1960, Stresses in shells
[7]   The nonlinear prebuckling response of short thin-walled laminated composite cylinders in bending [J].
Fuchs, HP ;
Hyer, MW .
COMPOSITE STRUCTURES, 1996, 34 (03) :309-324
[8]  
GAVELYA SP, 1986, PRIKL MEKH, V22, P63
[9]  
HU S, 1994, COMPOS SCI TECHNOL, V47, P321
[10]  
*IMSL MATH, 1987, LIBR US MAN, P660