CORDIS Project
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This project focuses on wind tunnel testing of a new helicopter rotor design featuring Active Gurney Flaps. The research will evaluate rotor performance under various flight conditions using advanced techniques like Particle Image Velocimetry to analyze airflow over the blades.
The project pertains to the wind tunnel testing of an innovative helicopter rotor with Active Gurney Flaps on the blades.
The experiments will be carried out in a facility highly specialised for helicopter model testing.
The effects of the flap on rotor performances will be assessed in different operating conditions of the rotor, including both hover and forward flight conditions. A particular feature of the experimental set up will be the Particle Image Velocimetry (PIV) system. PIV will be use…
POLITECNICO DI MILANO
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