通过引入哈密顿体系,将临界载荷和临界温度及它们所对应的屈曲模态归结为辛体系下的广义本征值和本征解问题。根据辛本征解的正交性和完备性,给出了全部的且独立存在的屈曲模态。数值结果表明,在轴向冲击载荷和温度耦合作用下,弹性圆柱壳的屈曲呈现出复杂的模式,温度直接影响冲击临界载荷的大小。随着温度的增加,冲击临界荷载降低,最后,文中给出各种条件下的屈曲模态。
In this paper,Hamiltonian system is introduced.In the system,the critical impact loads,critical temperatures and their buckling modes of the problem are reduced to the problems of generalized eigenvalues and eigensolutions respectively.Since the symplectic space of eigensolutions is complete and there are adjoint relationships of the symplectic ortho-normalization between the eigensolutions,all buckling modes,which exist independently,are shown.Numerical results show that buckling modes of elastic cylindrical shells are complicated under axial impact coupling with thermal loads.The temperature can change the critical values of the impact load.Namely,critical impact loads decrease with the temperature getting the higher.Some buckling modes are given under various conditions.