Numerical Estimation of Weight Efficiency for Aircraft Composite Lattice Shells with Grid Parameter Variable over Height
- Autores: Bokuchava P.1, Evstaf’ev V.1, Babuk V.1
-
Afiliações:
- Ustinov Baltic State Technical University “Voenmekh”
- Edição: Volume 62, Nº 1 (2019)
- Páginas: 1-4
- Seção: 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
Citar
Resumo
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.
Palavras-chave
Sobre autores
P. Bokuchava
Ustinov Baltic State Technical University “Voenmekh”
Autor responsável pela correspondência
Email: bokuchava.peter@yandex.ru
Rússia, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Evstaf’ev
Ustinov Baltic State Technical University “Voenmekh”
Email: bokuchava.peter@yandex.ru
Rússia, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Babuk
Ustinov Baltic State Technical University “Voenmekh”
Email: bokuchava.peter@yandex.ru
Rússia, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005