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Aeroacoustic Investigation of a High-Lift Device by Means of Simultaneous PIV and Microphone Array Measurements

Henning, Arne (2012) Aeroacoustic Investigation of a High-Lift Device by Means of Simultaneous PIV and Microphone Array Measurements. Journal of Sound and Vibration, Vol. 331 (2, 2.1), pp. 4610-4611. Elsevier, ScienceDirect. DOI: 10.1016/j.jsv.2012.05.012. ISSN 0022-460X.

Full text not available from this repository.

Official URL: http://www.elsevier.com

Abstract

The noise sources at the leading edge slat in a high-lift device configuration are investigated by means of the causality correlation method. The calculated cross-correlation between the acoustic far-field pressure and near-field fluctuations obtained via particle image velocimetry (PIV) provides information about the flow structures which are part of the sound generation process.

Document Type:Article
Additional Information:Beitrag zum Artikel: Review, Aeroacousticsresearch in Europe: The CEAS-ASC report on 2011 highlights, A. McAlpine *, R.J. Astley, Institute of Sound and Vibration Research, University of Southampton, Highfield, Southampton, SO171BJ, UK
Title:Aeroacoustic Investigation of a High-Lift Device by Means of Simultaneous PIV and Microphone Array Measurements
Authors:
AuthorsInstitution or Email of Authors
Henning, ArneTU-Berlin
Date:2012
Journal or Publication Title:Journal of Sound and Vibration
Refereed publication:Yes
In Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol. 331
DOI:10.1016/j.jsv.2012.05.012
Page Range:pp. 4610-4611
Publisher:Elsevier, ScienceDirect
Series Name:Aeroacoustics research in Europe: The CEAS-ASC report on 2011 Highlights
ISSN:0022-460X
Status:Published
Keywords:Microphone Array, PIV
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation & Validation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:17 Jul 2012 12:07
Last Modified:07 Feb 2013 20:35

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