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DSpace at Transilvania University >
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COMAT 2010 >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/123456789/1267
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| Title: | OPTIMIZATION OF ADAPTIVE WING SKIN COMPOSITE MATERIAL USING FEM |
| Authors: | NICULITA, Camelia
VLASE, Sorin
BORITU, Andreea
BENCZE, A. |
| Keywords: | plate
skin
wing
model
displacement
stress |
| Issue Date: | Oct-2010 |
| Publisher: | Transilvania University Press of Braşov |
| Citation: | GOOGLE SCHOLAR |
| Series/Report no.: | COMAT 2010;157-162 |
| Abstract: | The paper is presenting a finite element modeling of a plate, the purpose of the calculation being to define a composite material which can be used for skin at an adaptive wing, so can be obtain shape changing’s: maximum displacement and minimum stresses. Use of software is essential in the evolution of engineering. In aviation products must provide performance and reliability at the highest level. Also, the use of software aims to reduce costs in design, implementation and operation. |
| URI: | http://hdl.handle.net/123456789/1267 |
| ISSN: | 1844 - 9336 |
| Appears in Collections: | COMAT 2010
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