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- Article name
- Numerical stability analysis of aircraft composite lattice cylindrical shells with changing quantity of annular ribs
- Authors
- EVSTAFYEV V. A., , virata@rambler.ru, Baltic State Technical University "VOENMEH" named after D. F. Ustinov, Saint-Petersburg, Russia
BOKUCHAVA P. N., , haxsender@ya.ru, Baltic State Technical University "VOENMECH" named after D. F. Ustinov, St.-Petersburg, Russia
BABUK V. A., , babuk@peterlink.ru, Baltic State Technical University "VOENMECH" named after D. F. Ustinov, St.-Petersburg, Russia
- Keywords
- lattice structures / composite materials / analysis / stability
- Year
- 2015 Issue 4 Pages 3 - 5
- Code EDN
- Code DOI
- Abstract
- The stability of carbon-epoxy composite lattice cylindrical shell loaded with longitudinal compressive and shear forces at the upper end with annular ribs with quantity changes by height was investigated by using the ANSYS package. The results can be used in the design of similar structures.
- Text
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