Abstract
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.
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Makhnovich, S.V., Permyakov, D.A., Khishchenko, Y.M. (2020). Deformation and Stability of Cylindrical Shells Under Irregular Radial Loading. In: Radionov, A., Kravchenko, O., Guzeev, V., Rozhdestvenskiy, Y. (eds) Proceedings of the 5th International Conference on Industrial Engineering (ICIE 2019). ICIE 2019. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-22041-9_17
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