Objetivo "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." Ámbito científico engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftrotorcraft Programa(s) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Tema(s) JTI-CS-2011-2-GRC-01-006 - Wind Tunnel Testing of Active Rotor Convocatoria de propuestas SP1-JTI-CS-2011-02 Consulte otros proyectos de esta convocatoria Régimen de financiación JTI-CS - Joint Technology Initiatives - Clean Sky Coordinador POLITECNICO DI MILANO Aportación de la UE € 341 550,00 Dirección PIAZZA LEONARDO DA VINCI 32 20133 Milano Italia Ver en el mapa Región Nord-Ovest Lombardia Milano Tipo de actividad Higher or Secondary Education Establishments Contacto administrativo Franco Bernelli Zazzera (Prof.) Enlaces Contactar con la organización Opens in new window Sitio web Opens in new window Coste total Sin datos
