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

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(JTI-CS2-2016-CFP04-REG-01-05) - GREEN TURBOPROP - HIGH LIFT CONFIGURATION INTEGRATING ADAPTIVE WING CONCEPT - LOW SPEED EXPERIMENTAL VALIDATION

Programme: Horizon 2020 Framework Programme
Call: Clean Sky Call for Proposals 04 EU

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.

Keywords

HLD High Lift Devices WTT Wind tunnel Testing/Technology

Tags

Aerodynamics

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