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任意载荷下加筋旋转壳稳定性分析的半解析有限元
A SEMIANALYTICAIL FINITE ELEMENT FOR BUCKLING ANALYSIS OF STIFFENED SHELL OF REVOLUTION UNDER ARBITRARY LOADS
【摘要】 <正> 本文推导了一个半解析加筋锥壳元(图1)的线性刚阵和几何刚阵,该元可用于加筋旋转壳在任意载荷下的弹性稳定性分析。规定环向筋条和纵向筋条分别置于壳元的母线和周线上。
【Abstract】 The linear and geometric stiffness matrices of a semianalytical stiffened conical shell element are derived in this paper. This element can be used for elastic buckling analysis of a stiffened shell of revolution under arbitrary loads, Two numerical examples are analyzed and the results show that this element is available.
- 【文献出处】 航空学报 ,Acta Aeronautica Et Astronautica Sinica , 编辑部邮箱 ,1987年06期
- 【被引频次】1
- 【下载频次】40