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Open AccessProceedings ArticleDOI

Flyover Noise Measurements on Landing Aircraft with a Microphone Array

TLDR
In this paper, the noise sources of landing commercial aircraft were examined with planar arrays consisting of 96 or 111 microphones mounted on an 8 m by 8 m plate under the glide path on the ground.
Abstract
The noise sources of landing commercial aircraft were examined with planar arrays consisting of 96 or 111 microphones mounted on an 8 m by 8 m plate under the glide path on the ground. It is shown that important airframe noise sources can be identified in spite of the presence of engine noise, i.e., landing-gear noise, flap side-edge noise, flap-gap noise, jet-flap interaction noise, slat-horn noise, slat-track noise. A surprising finding is a noise source near the wing tips of some aircraft which is tentatively called wake-vortex wing interaction noise. It is shown to be the by far strongest noise source (6 dB(A) louder than the engines) on a regional jet aircraft.

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Citations
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Plasma Actuators for Cylinder Flow Control and Noise Reduction

TL;DR: In this article, the results of flow-control experiments using single dielectric barrier discharge plasma actuators to control flow separation and unsteady vortex shedding from a circular cylinder in crossflow are reported.
Proceedings ArticleDOI

Effect of Directional Array Size on the Measurement of Airframe Noise Components

TL;DR: In this article, the effects of overall size of directional arrays on the measurement of aeroacoustic components were examined in the potential core of an open-jet windtunnel, with the directional arrays located outside the flow in an anechoic environment.
Journal ArticleDOI

Time-Accurate Simulations and Acoustic Analysis of Slat Free Shear Layer

TL;DR: In this article, a spatiotemporal resolution of the free shear layer in the slat-cove region is used to obtain the farfield acoustics of a multi-element, high-lift configuration.
Proceedings ArticleDOI

Location of rotating sources by phased array measurements

TL;DR: In this paper, a method for the location of moving sources by a microphone array is described, which can be applied to out-of-flow measurements in an open jet wind tunnel.
References
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Proceedings ArticleDOI

Airframe Noise Studies on Wings with Deployed High Lift Devices

TL;DR: In this article, an acoustic mirror was employed on a 1/10 scale-model wing section to identify the aeroacoustic source mechanisms of slat-noise and flap side-edge noise.
Journal ArticleDOI

Wheel/rail noise generated by a high-speed train investigated with a line array of microphones

TL;DR: In this paper, the effect of wheel-noise absorbers and freshly turned treads on radiated noise on a high-speed electric train travelling at speeds up to 250 km/h was investigated.
Journal ArticleDOI

Experiences with various configurations of microphone arrays used to locate sound sources on railway trains operated by the db ag

TL;DR: In this paper, an overview of the results and conclusions from measurements made with various configurations of microphone arrays designed to locate sound sources on trains operated by the Deutsche Bahn AG at speeds up to 280 km/h.
Proceedings ArticleDOI

Airframe noise source localization using a microphone array

TL;DR: In this article, a new phased array processing method was developed to achieve accurate two-dimensional localization of acoustic sources, which is designed for sparse arrays, and uses many fewer microphones.
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It is shown that important airframe noise sources can be identified in spite of the presence of engine noise, i. e., landing-gear noise, flap side-edge noise, flap-gap noise, jet-flap interaction noise, slat-horn noise, slat-track noise.