Skip to main content

Advanced european tiltrotor dynamics and noise

Objective

The project is intended to enhance the EU knowledge on tilt rotor technologies by deeply analyzing the Whirl-Flutter, an aero elastic instability of the rotor/pylon system occurring at high inflow speeds typical of tilt rotors. The research is conducted by a comparison of analytical and experimental results. Tests will be done in a high-speed wind tunnel facility using a half-span scaled model. The availability of a wind tunnel model that is useful also for aero acoustic analysis will help optimize the rotor blade design for a low external noise level and, at the same time, a performance assessment in wind tunnel will demonstrate the validity of this design in all flight conditions. The project will provide final recommendations for the design of a full-scale tilt rotor flight demonstrator (ERICA).

Call for proposal

Data not available

Coordinator

AGUSTA S.P.A.
Address
Via Giovanni Agusta 520
21017 Samarate
Italy

See on map

Participants (7)

CENTRO ITALIANO RICERCHE AEROSPAZIALI S.C.P.A.
Italy
Address
Via Maiorise
81043 Capua

See on map

EUROCOPTER DEUTSCHLAND GMBH
Germany
Address

81663 Muenchen

See on map

EUROCOPTER S.A.S.
France
Address
Aeroport International Marseille
13725 Marignane

See on map

IDS INGEGNERIA DEI SISTEMI SPA
Italy
Address
Via Livornese 1019
56010 Pisa

See on map

NATIONAL TECHNICAL UNIVERSITY OF ATHENS*ETHNICON METSOVION POLYTECHNION
Greece
Address
Heroon Polytechniou Str. , 9
15773 Athens

See on map

POLYTECHNIC OF MILAN
Italy
Address
Via La Masa 34
20156 Milano

See on map

STICHTING NATIONAAL LUCHT- EN RUIMTEVAART LABORATORIUM
Netherlands
Address
2,anthony Fokkerweg 2
1059 CM Amsterdam

See on map