Deformation of an Elongated Thin-Shell Structure with a Dynamically Fracturing Thermal Protection Coating
- 作者: Antuf’ev B.A.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 61, 编号 4 (2018)
- 页面: 505-508
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230672
- DOI: https://doi.org/10.3103/S1068799818040013
- ID: 230672
如何引用文章
详细
An approximate solution of the problem of dynamic deformation of an elongated thinshell structure with a fracturing thermal protection coating is given. The paper investigates how the structure frequencies change over the entire process of fracture. Examples are given.
作者简介
B. Antuf’ev
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: antufjev.bor@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
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