This paper presents the key objectives from an European Union funded collaborative project investigating the noise installation effects for novel regional advanced aircraft concepts using Open Rotor (OR) propulsion systems. The consortium for the project:WENEMOR, will address the topic by carrying out aero-acoustic measurements in the open test section of a large low speed wind tunnel using a complete reduced scale modular model of different configurations of an aircraft with installed counter rotating open rotor systems operating in both pusher and tractor modes. The principal goal of the project is to assess experimentally the noise shielding effectiveness of classic airframe components for different Open Rotor aircraft configurations. A complete 1/7th scale aircraft has been designed and built for installation in the Pininfarina Aerodynamic and Aeroacoustic Research Center Wind Tunnel. The model has two Open Rotors with a contra-rotating fan at the same scale as the airframe. Various positions of the ORs with respect to the airframe will be tested with noise measurements being performed both in the near and the far field. The test campaign will provide, for the first time in Europe, a comprehensive database on noise installation effects for novel regional advanced aircraft concepts using OR propulsion systems. Two accompanying conference papers present preliminary results

WENEMOR: Wind tunnel tests for the evaluation of the installation effects of noise emissions of an open rotor advanced regional aircraft / Bennett, Gareth J.; Kenned, John; Eret, Petr; Cappadona, Filippo; Bianco, Antonello; Letizia, Raffaele; Danise, Davide; Lamotte, Lucille; Picard, Christophe; Finez, Arthur; Castellini, Paolo; Chiariotti, Paolo; Sopranzetti, Francesca; Tsahalis, Demosthenis; Tsahalis, Haralabos; Moussas, Vassilios; Paonessa, Antonio; Amoroso, Francesco; Di Giulio, Massimiliano. - (2013), p. 90. (Intervento presentato al convegno 19th AIAA/CEAS Aeroacoustics Conference tenutosi a Berlin, deu nel 2013).

WENEMOR: Wind tunnel tests for the evaluation of the installation effects of noise emissions of an open rotor advanced regional aircraft

AMOROSO, FRANCESCO;
2013

Abstract

This paper presents the key objectives from an European Union funded collaborative project investigating the noise installation effects for novel regional advanced aircraft concepts using Open Rotor (OR) propulsion systems. The consortium for the project:WENEMOR, will address the topic by carrying out aero-acoustic measurements in the open test section of a large low speed wind tunnel using a complete reduced scale modular model of different configurations of an aircraft with installed counter rotating open rotor systems operating in both pusher and tractor modes. The principal goal of the project is to assess experimentally the noise shielding effectiveness of classic airframe components for different Open Rotor aircraft configurations. A complete 1/7th scale aircraft has been designed and built for installation in the Pininfarina Aerodynamic and Aeroacoustic Research Center Wind Tunnel. The model has two Open Rotors with a contra-rotating fan at the same scale as the airframe. Various positions of the ORs with respect to the airframe will be tested with noise measurements being performed both in the near and the far field. The test campaign will provide, for the first time in Europe, a comprehensive database on noise installation effects for novel regional advanced aircraft concepts using OR propulsion systems. Two accompanying conference papers present preliminary results
2013
9781624102134
9781624102134
WENEMOR: Wind tunnel tests for the evaluation of the installation effects of noise emissions of an open rotor advanced regional aircraft / Bennett, Gareth J.; Kenned, John; Eret, Petr; Cappadona, Filippo; Bianco, Antonello; Letizia, Raffaele; Danise, Davide; Lamotte, Lucille; Picard, Christophe; Finez, Arthur; Castellini, Paolo; Chiariotti, Paolo; Sopranzetti, Francesca; Tsahalis, Demosthenis; Tsahalis, Haralabos; Moussas, Vassilios; Paonessa, Antonio; Amoroso, Francesco; Di Giulio, Massimiliano. - (2013), p. 90. (Intervento presentato al convegno 19th AIAA/CEAS Aeroacoustics Conference tenutosi a Berlin, deu nel 2013).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/659136
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