COUPLED TRANSIENT ANALYSIS OF A UAV COMPOSITE WING.

Autor: Ştefan, Amado, Larco, Ciprian, Pahonie, Radu-Călin, Nicolaescu, Ionuț
Předmět:
Zdroj: Proceedings of the Scientific Conference AFASES; May2015, Vol. 2, p481-486, 6p
Abstrakt: This article focuses on the flexibility influence over aerodynamic forces on a mini-airplane wing. For the flow around the flexible wing a transient structural analysis and a CFD analysis were coupled. The results were compared with the CFD analysis over a rigid wing structure. [ABSTRACT FROM AUTHOR]
Databáze: Complementary Index