Rotating blade trailing-edge noise : experimental validation of analytical model - Archive ouverte HAL Accéder directement au contenu
Article Dans Une Revue AIAA Journal Année : 2010

Rotating blade trailing-edge noise : experimental validation of analytical model

Résumé

This paper deals with the experimental validation of an analytical trailing-edge noise model dedicated to low-speed fans operating in free field. The model is intrinsically related to the aerodynamics of the blades and should lead to a useful fast-running tool to be included in a blade-design process in an industrial context. The investigations are made on a two-bladed low-speed axial fan without shroud, installed inside an anechoic room. The blades are instrumented with two sets of embedded small-size microphones (2.5 mm diam), and the wall-pressure signals are acquired via a slip ring mounted on the fan axis. The chord-based Reynolds number is about 200,000, and the tip Mach number about 0.07. The data base is completed by far-field measurements made with a single microphone on a moving support. The analytical model is based on a previously published extension of Amiet's trailing-edge noise theory. A blade is split into several strips in the spanwise direction, and the model is applied to each strip. For this the input data are interpolated from the measurements performed with the aforementioned sets of microphones. The trailing-edge noise model is more reliable for observer positions within ±30° from the fan-rotation plane.
Fichier principal
Vignette du fichier
AIAAj_2008.pdf (6.18 Mo) Télécharger le fichier
Origine : Fichiers produits par l'(les) auteur(s)
Loading...

Dates et versions

hal-00566059 , version 1 (08-03-2012)

Identifiants

Citer

Yannick Rozenberg, Michel Roger, Stéphane Moreau. Rotating blade trailing-edge noise : experimental validation of analytical model. AIAA Journal, 2010, 48, pp.951-962. ⟨10.2514/1.43840⟩. ⟨hal-00566059⟩
259 Consultations
915 Téléchargements

Altmetric

Partager

Gmail Facebook X LinkedIn More