Deformation and Stability of Cylindrical Shells Under Irregular Radial Loading

被引:0
作者
Makhnovich, S., V [1 ]
Permyakov, D. A. [1 ]
Khishchenko, Yu M. [1 ]
机构
[1] South Ural State Univ, 76 Lenin Av, Chelyabinsk 454080, Russia
来源
PROCEEDINGS OF THE 5TH INTERNATIONAL CONFERENCE ON INDUSTRIAL ENGINEERING, ICIE 2019, VOL I | 2020年
关键词
Orthotropic shell; Irregular loading; Bearing pressures; Asymmetric deformation; Shell stability; Comparison with an experiment;
D O I
10.1007/978-3-030-22041-9_17
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The article considers a non-axisymmetric deformation and stability of a compressed aircraft shell. Particular attention is paid to modeling contact interaction of shells with transverse shock-absorbing belts. To analyze shell deformations, we used the iteration method, taking into account a nonlinear change in the reaction of the shock-absorbing belt when there are structure displacements. The shell stability equations were discretized by the Bubnov-Galerkin method using Fourier series. The developed model was used to study the deformation mode of constructively and technologically orthotropic shells exposed to local loads of shock-absorbing belts. The simulation models were verified with the results of testing model and actual shells.
引用
收藏
页码:145 / 158
页数:14
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