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Green Turboprop - High lift configuration integrating adaptive wing concept - Low Speed experimental validation
Deadline: Oct 5, 2016  

 Aerospace Technology
 Aeronautics Industries
 Horizon Europe

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.

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