Green Turboprop - High lift configuration integrating adaptive wing concept - Low Speed experimental validation

Date de clôture : 5 oct. 2016  
APPEL À PROJET CLÔTURÉ

Topic Description

Specific Challenge:

Low Speed Experimental Investigation of a Large scale complete aircraft model integrating different High lift morphing devices. Activities include modifications of an existing large scale A/C model (scale 1:7) to include new morphing high lift device shapes (droop nose, fowler flaps) and to validate the relevant aerodynamic performances at A/C level.

Lien officiel :   Disponible pour les utilisateurs enregistrés