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Autor:
Andreea KOREANSCHI, Mehdi ben HENIA, Olivier GUILLEMETTE, Francois MICHAUD, Yvan TONDJI, Oliviu SUGAR GABOR, Ruxandra Mihaela BOTEZ, Manuel FLORES SALINAS
Publikováno v:
INCAS Bulletin, Vol 8, Iss 1, Pp 99-124 (2016)
As part of a morphing wing technology project, the flutter analysis of two finite element models and the experimental results of a morphing wing demonstrator equipped with aileron are presented. The finite element models are representing a wing secti
Externí odkaz:
https://doaj.org/article/b40c5d850b694333b1c28b49f9526403