To obtain access to full text of journal and articles you must register!
- Article name
- Numerical analysis of the influence of the longitudinal ribs quantity and location on aircraft composite lattice cylindrical shells mass
- Authors
- EVSTAFYEV V. A., , virata@rambler.ru, Baltic State Technical University "VOENMEH" named after D. F. Ustinov, Saint-Petersburg, Russia
BABUK V. A., , babuk@peterlink.ru, Baltic State Technical University "VOENMECH" named after D. F. Ustinov, St.-Petersburg, Russia
BOKUCHAVA P. N., , bokuchava.peter@ya.ru, Baltic State Technical University "VOENMEH" name after D. F. Ustinov, St.-Petersburg, Russia
- Keywords
- lattice structures / composite materials / analysis / stability
- Year
- 2018 Issue 3 Pages 19 - 22
- Code EDN
- Code DOI
- Abstract
- Using the ANSYS package the influence of the quantity and displacement of longitudinal ribs of carbon-epoxy composite lattice cylindrical shell on their mass was investigated in cases where stability or rigidity constraints exist. In the first case the shells were loaded with longitudinal compressive and shear forces. In the second the concentrated mass was fixed on the edge of the shell. The results can be used in the design of similar structures.
- Text
- To obtain access to full text of journal and articles you must register!
- Buy
