scispace - formally typeset
Open Access

Leading edge serrations which reduce the noise of low-speed rotors

Reads0
Chats0
TLDR
In this article, the serrations were used as noise suppressors at rotor tip speeds less than 135 m/sec (444 ft/sec) than at higher speeds for two different size rotors.
Abstract
Acoustic effects of serrated brass strips attached near the leading edges of two different size rotors were investigated. The two bladed rotors were tested in hover. Rotor rotational speed, blade angle, serration shape, and serration position were varied. The serrations were more effective as noise suppressors at rotor tip speeds less than 135 m/sec (444 ft/sec) than at higher speeds. high frequency noise was reduced but the low frequency rotational noise was little affected. Noise reductions from 4 to 8 db overall sound pressure level and 3 to 17 db in the upper octave bands were achieved on the 1.52 m (5.0 ft) diameter rotor. Noise reductions up to 4 db overall sound pressure level were measured for the 2.59 m (8.5 ft) diameter rotor at some conditions.

read more

Citations
More filters
Journal ArticleDOI

Airfoil noise reductions through leading edge serrations

TL;DR: In this article, the effect of LE serrations on noise reduction was investigated on a flat plate in an open jet wind tunnel and the results showed that the amplitude of the LE amplitude was a key parameter for enhancing the noise reduction.
Journal ArticleDOI

Experimental and numerical investigation of turbulence-airfoil noise reduction using wavy edges

TL;DR: In this article, a passive leading-edge treatment based on sinusoidal serrations aimed at reducing turbofan interaction noise has been recently studied in the framework of a European project (FLOCON), where the turbulence-airfoil interaction mechanism is achieved using a turbulence grid located upstream of an isolated NACA airfoil tested in anechoic open jet wind tunnel.
Journal ArticleDOI

Vortex shedding noise of low tip speed, axial flow fans

TL;DR: In this paper, the authors conducted noise and performance tests on three low tip speed, half-stage, axial flow fans to determine the nature of the vortex shedding noise mechanism, which is due to instabilities in the laminar boundary layer on the suction side of the blade where these instabilities are in the form of Tollmien-Schlichting (T-S) waves.
Journal ArticleDOI

Investigation of Acoustic Effects of Leading-Edge Serrations on Airfoils

TL;DR: In this article, a series of extensive studies of the application of leading edge serrations as a device for reducing the vortex noise radiated from stationary and rotating airfoils in low Reynolds number flow are presented and interpreted.
Journal ArticleDOI

Morphometric characterisation of wing feathers of the barn owl Tyto alba pratincola and the pigeon Columba livia

TL;DR: The quantitative description of the feathers and the specific structures of owl feathers can be used as a model for the construction of a biomimetic airplane wing or, in general, as a source for noise-reducing applications on any surfaces subjected to flow fields.
Related Papers (5)