Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws.

Autor:	Cestino, E., Frulla, G.1, Perotto, E.2, Marzocca, P.3
Zdroj:	Journal of Aerospace Engineering. Jan/Feb2014, Vol. 27 Issue 1, p112-120. 9p.
Databáze:	Academic Search Ultimate
Externí odkaz:	Zobrazit plný text záznamu