航空学报 > 1984, Vol. 5 Issue (1): 37-45

锥形薄壳的弹性稳定性

赵金德   

  1. 上海飞机研究所
  • 收稿日期:1982-11-01 修回日期:1900-01-01 出版日期:1984-03-25 发布日期:1984-03-25

ELASTIC STABILITY OF CONICAL SHELLS

Zhao Jinde   

  1. Shanghai Aircraft Research Institute
  • Received:1982-11-01 Revised:1900-01-01 Online:1984-03-25 Published:1984-03-25

摘要: 本文用变分原理推导了锥形薄壳稳定性的基本微分方程式。在推导过程中,考虑了壳体微元在中面内的变形和绕各个轴的转动。所得的方程最后化为用三个位移表达的微分方程式,它适用于各种载荷情况,并避免了“唐纳尔型”方程的限制和出于物理想像来建立锥形壳微分方程式的错觉。作为本文理论应用的一个例子,最后用伽辽金方法近似解答了全锥在外压作用下的稳定性问题,获得了简洁的临界压力计算公式。所得结果与实验一致。

Abstract: The basic differentia] equations of the conical thin shells are derived by the variational principle. The deformations of the element in the middle surface of the shell and its rotation about all axes are considered in the derivation of these equations. Finally, they are deduced to three differential equations in terms of the displacements, which can be applied to any loaded case without the restraints of the "Donnell-type" equations and the illusions in establishment of the differential equations of conical shells based on the pure physical intuitions.As an numerical example, a buckling problem of a complete cone under external pressure is solved by the Galerkin's method and a simple formula for the critical pressure is obtained. The results are in good agreement w ith the experimental data.