Email this article Numerical Estimation of Weight Efficiency for Aircraft Composite Lattice Shells with Grid Parameter Variable over Height
- Authors: Bokuchava P.N.1, Evstaf’ev V.A.1, Babuk V.A.1
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Affiliations:
- Ustinov Baltic State Technical University “Voenmekh”
- Issue: Vol 62, No 1 (2019)
- Pages: 1-4
- Section: 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
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Abstract
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.
About the authors
P. N. Bokuchava
Ustinov Baltic State Technical University “Voenmekh”
Author for correspondence.
Email: bokuchava.peter@yandex.ru
Russian Federation, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. A. Evstaf’ev
Ustinov Baltic State Technical University “Voenmekh”
Email: bokuchava.peter@yandex.ru
Russian Federation, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. A. Babuk
Ustinov Baltic State Technical University “Voenmekh”
Email: bokuchava.peter@yandex.ru
Russian Federation, ul. 1-ya Krasnoarmeiskaya 1, St. Petersburg, 190005
