GUM

Active GUrney on Main Rotor blades

 Coordinatore POLITECNICO DI MILANO 

 Organization address address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133

contact info
Titolo: Prof.
Nome: Franco
Cognome: Bernelli Zazzera
Email: send email
Telefono: 390224000000
Fax: 390224000000

 Nazionalità Coordinatore Italy [IT]
 Totale costo 455˙401 €
 EC contributo 341˙550 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2011-02
 Funding Scheme JTI-CS
 Anno di inizio 2012
 Periodo (anno-mese-giorno) 2012-03-01   -   2015-12-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    POLITECNICO DI MILANO

 Organization address address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133

contact info
Titolo: Prof.
Nome: Franco
Cognome: Bernelli Zazzera
Email: send email
Telefono: 390224000000
Fax: 390224000000

IT (MILANO) coordinator 341˙550.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

helicopter    piv    blades    wind    flow    active    innovative    rotor    tunnel    surveys   

 Obiettivo del progetto (Objective)

'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.'

Introduzione (Teaser)

Active control of wind flow over rotorcraft could be an important way to reduce fuel consumption while enhancing performance. EU-funded scientists have developed a non-invasive test for wind tunnel-evaluation of a promising technology.

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