Shell analysis of an inflatable arch subjected to snow and wind loading

被引:31
作者
Plaut, RH [1 ]
Goh, JKS
Kigudde, M
Hammerand, DC
机构
[1] Virginia Polytech Inst & State Univ, Charles E Via Jr Dept Civil & Environm Engn, Blacksburg, VA 24061 USA
[2] Virginia Polytech Inst & State Univ, Dept Aerosp & Ocean Engn, Blacksburg, VA 24061 USA
关键词
arches; elastic; energy methods; Rayleigh-Ritz method; Sanders theory; shell; snow load; wind load;
D O I
10.1016/S0020-7683(99)00189-4
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A flexible material, such as a woven or braided fabric, may be tailored to form an arch when inflated. Such arches have been used as the framework for transportable shelters and are analyzed in this paper. It is assumed that the cross section of the pressurized arch is circular and that only in-plane (membrane) stresses are present. An analytical solution for these initial stresses is given for an arbitrary arch centerline shape. Then external loads are applied, and the additional stress resultants include bending and twisting moments. The linear thin-shell theory of Sanders is used to formulate the governing equations, including the effect of the initial membrane stresses. The material is linearly elastic, nonhomogeneous, and orthotropic. Approximate solutions are obtained using the Rayleigh-Ritz method. In the examples, the centerline of the arch is a semi-circle, the ends are fixed, and the material is homogeneous and isotropic. Four loads are treated: a symmetric ('full') snow load, an asymmmetric ('half) snow load, a wind load symmetric with respect to the plane of the arch centerline, and a distributed load acting sideways. The resulting deflections are computed and plotted. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:4275 / 4288
页数:14
相关论文
共 32 条
[1]   NUMERICAL ANALYSIS OF UNSYMMETRICAL BENDING OF SHELLS OF REVOLUTION [J].
BUDIANSKY, B ;
RADKOWSKI, PP .
AIAA JOURNAL, 1963, 1 (08) :1833-1842
[2]  
Budiansky B, 1963, PROGR SOLID MECH PRA, P129
[3]  
Carradine D. M., 1998, INT J SPACE STRUCTUR, V13, P197
[4]  
Chow P.Y., 1992, J AEROSPACE ENG, V5, P274, DOI 10.1061/(ASCE)0893-1321(1992)5:3(274)
[5]  
DENT RN, 1972, PRINCIPLES PNEUMATIC
[6]  
GALAS B, 1998, FABRICS ARCHITECTURE, V10, P19
[7]  
HAMPEL JW, 1996, P 20 ARM SCI C SCI T, V2, P953
[8]  
Jones RM, 1999, MECH COMPOSITE MAT
[9]  
Kawaguchi M., 1996, LIGHT STRUCTURES STR
[10]  
KAWAGUCHI M, 1972, TENSION STRUCTURES S, P449