轴向阶梯载荷下薄圆柱壳的弹性动力屈曲

ELASTIC DYNAMIC BUCKLING OF THIN CYLINDRICAL SHELLS SUBJECT TO AXIAL STEP LOAD

  • 摘要: 对于轴向阶梯载荷下圆柱壳的非轴对称动力屈曲,将临界应力和屈曲惯性指数作为双特征参数求解.由屈曲瞬间的能量转换和守恒准则导出压缩波阵面上的屈曲变形补充约束方程.利用Galerkin方法求解失稳控制方程,得出包含双特征参数的代数特征值问题.该特征值问题满足补充约束方程的解给出动力屈曲的临界应力和惯性指数.

     

    Abstract: Critical stress and inertial exponent are treated as two characteristic parameters for the asymmetric dynamic buckling of cylindrical shells under axial step loading.The supplementary restraint equation of buckling deformation at compressive wave front is derived by the use of the criterion of transformation and conservation of energy in the transient buckling process.The Galerkin method is used to solve the governing equations,and the algebraic eigenvalue problem including the two characteristic parameters is obtained.On condition that the supplementary restraint equation is satisfied,the solution of the eigenvalue problem gives the values of the critical stress and the inertial exponent for the dynamic buckling.

     

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