Numerical Estimation of Weight Efficiency for Aircraft Composite Lattice Shells with Grid Parameter Variable over Height
- 作者: Bokuchava P.1, Evstaf’ev V.1, Babuk V.1
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隶属关系:
- Ustinov Baltic State Technical University “Voenmekh”
- 期: 卷 62, 编号 1 (2019)
- 页面: 1-4
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230804
- DOI: https://doi.org/10.3103/S106879981901001X
- ID: 230804
如何引用文章
详细
The influence of grid parameters variable over height on the weight of cylindrical and conical lattice shells made of carbon fiber is studied using the ANSYS software. The shells are loaded with longitudinal compressive and shear forces on the upper end face.
作者简介
P. Bokuchava
Ustinov Baltic State Technical University “Voenmekh”
编辑信件的主要联系方式.
Email: bokuchava.peter@yandex.ru
俄罗斯联邦, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Evstaf’ev
Ustinov Baltic State Technical University “Voenmekh”
Email: bokuchava.peter@yandex.ru
俄罗斯联邦, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Babuk
Ustinov Baltic State Technical University “Voenmekh”
Email: bokuchava.peter@yandex.ru
俄罗斯联邦, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005