Design and manufacturing of a large-scale HLFC wing model for a transonic WTT

The main purpose of this topic is to design and manufacture (instrumentation included) a large wing-model which will be equipped with wall-suction parts in the leading-edge region in order to perform Hybrid Laminar Flow Control (HLFC) by using active and passive suction systems. The ultimate objective (not included in the scope of this topic) is to perform Wind-Tunnel Tests (WTT) of the model inside a large transonic facility in order to prove the aerodynamic efficiency and the robustness of active and passive HLFC technologies under transonic flow conditions. Please refer to the full topic descriptions document published in this call.