Objectif "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 used to carry out some flow field surveys over the blades in order to achieve a better physical insight into the flow behaviour. Moreover, an innovative technique, further developing some recent approaches purposedin the literature, will be used to reconstruct the pressure distribution over the blade section on the base of proper PIV surveys." Champ scientifique engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftrotorcraft Programme(s) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Thème(s) JTI-CS-2011-2-GRC-01-006 - Wind Tunnel Testing of Active Rotor Appel à propositions SP1-JTI-CS-2011-02 Voir d’autres projets de cet appel Régime de financement JTI-CS - Joint Technology Initiatives - Clean Sky Coordinateur POLITECNICO DI MILANO Contribution de l’UE € 341 550,00 Adresse PIAZZA LEONARDO DA VINCI 32 20133 Milano Italie Voir sur la carte Région Nord-Ovest Lombardia Milano Type d’activité Higher or Secondary Education Establishments Contact administratif Franco Bernelli Zazzera (Prof.) Liens Contacter l’organisation Opens in new window Site web Opens in new window Coût total Aucune donnée
