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Active GUrney on Main Rotor blades

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 purposed
in the literature, will be used to reconstruct the pressure distribution over the blade section on the base of proper PIV surveys."

Appel à propositions

SP1-JTI-CS-2011-02
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Coordinateur

POLITECNICO DI MILANO
Contribution de l’UE
€ 341 550,00
Adresse
PIAZZA LEONARDO DA VINCI 32
20133 Milano
Italie

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Région
Nord-Ovest Lombardia Milano
Type d’activité
Higher or Secondary Education Establishments
Contact administratif
Franco Bernelli Zazzera (Prof.)
Liens
Coût total
Aucune donnée