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复合材料加筋圆锥壳的大变形方程
引用本文:王虎,王俊奎.复合材料加筋圆锥壳的大变形方程[J].航空学报,1990,11(5):271-276.
作者姓名:王虎  王俊奎
作者单位:北京航空航天大学 (王虎),北京航空航天大学(王俊奎)
摘    要: <正> 本文利用最小势能原理和平均筋条刚度法,建立了在任意载荷作用下以一环向密加筋复合材料圆锥壳的大变形方程。所建立的Donnell型方程可作为研究圆锥壳许多具体力学问题的理论基础。对一些特殊情况,给出了简化方程。 1.基本假设和关系式 在本文理论推导过程中作如下基本假设:

关 键 词:复合材料壳体  加筋壳  圆锥壳  几何非线性  大挠度方程  

THE LARGE DEFLECTION EQUATIONS OF STIFFENED LAMINATED COMPOSITE CONICAL SHELLS
Beijing University of Aeronautics and astronautics Wang Hu and Wang Tsunkuei.THE LARGE DEFLECTION EQUATIONS OF STIFFENED LAMINATED COMPOSITE CONICAL SHELLS[J].Acta Aeronautica et Astronautica Sinica,1990,11(5):271-276.
Authors:Beijing University of Aeronautics and astronautics Wang Hu and Wang Tsunkuei
Institution:Beijing University of Aeronautics and astronautics Wang Hu and Wang Tsunkuei
Abstract:In this paper, a new theory is developed for large deflection of closely stiffened truncated laminated composite conical shells under arbitrary loads by using the variational calculus and smeared-stiffener theory. The most general bending-stretching coupling, the effect of eccentricity of stiffeners and initial deflection are considered. The new equations of the mixed type of the shell are obtained in terms of the transverse deflection and stress function and can be used to solve the problems of stress analysis, deflection, stability and vibration of the shell. The simplified equations are also given for some particular cases.
Keywords:composite shell  stiffened shell  conical shell  geom-etrical nonlinearity  large deflection equations    
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