Specific Challenge:Large scale wind tunnel experimental validation of a natural laminar flow flexible wing model (scale 1:3) integrating innovative morphing active devices (droop nose, morphing trailing edge, morphing winglet). WT Tests are planned in low speed and in “cruise conditions” to validate the relevant aerodynamic and aeroelastic performances at wing level. For the full topic description see the Call Text Document (Annex of Workplan) published with this call.
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