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- Article name
- Numerical stability analysis of aircraft composite lattice cylindrical shells with changing by height parameters
- Authors
- BOKUCHAVA P. N., , bokuchava.pn@astronomikon.ru, Baltic State Technical University "VOENMEH" named after D. F. Ustinov, Saint-Petersburg, Russia
EVSTAFYEV V. A., , virata@rambler.ru, Baltic State Technical University "VOENMEH" name after D. F. Ustinov, St.-Petersburg, Russia
BABUK V. A., , , Baltic State Technical University "VOENMEH" name after D. F. Ustinov, St.-Petersburg, Russia
- Keywords
- lattice structures / composite materials / aircrafts / analysis / stability
- Year
- 2014 Issue 4 Pages 5 - 7
- Code EDN
- Code DOI
- Abstract
- By using the ANSYS package, the stability of carbon-epoxy composite lattice cylindrical shell with annular ribs, with step or size changes by height, loaded with longitudinal compressive and shear forces at the upper end, was investigated. The results can be used in the design of similar structures.
- Text
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