National Acoustic Laboratories Library

An experimental study of airfoil tip vortex formation noise (Record no. 2676)

MARC details
000 -LEADER
fixed length control field nam a22 7a 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20170106150420.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 170106b xxu||||| |||| 00| 0 eng d
040 ## - CATALOGING SOURCE
Transcribing agency National Acoustics Laboratories
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Moreau, Danielle J.
245 ## - TITLE STATEMENT
Title An experimental study of airfoil tip vortex formation noise
520 3# - SUMMARY, ETC.
Summary, etc This paper explores the noise produced by three-dimensional vortex flow at the tip of an airfoil. This noise source is an important component of the noise produced by aircraft high-lift systems. To investigate tip vortex formation noise, aeroacoustic measurements have been taken of a finite airfoil with flat ended tip in an anechoic wind tunnel at a range of flow speeds and angles of attack. Sound maps taken with a beamforming array are presented to show contributions of flow at the airfoil tip to overall airfoil noise production. Tip noise spectral data are also included to provide information about the nature of the noise source and scaling laws are developed of the noise generation process to model the noise data.
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Con J Doolan
773 3# - HOST ITEM ENTRY
Relationship information Proceedings 9-11 November 2016, Brisbane, Australia
Title Acoustics 2016
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/538/p29.pdf?sequence=1&isAllowed=y">http://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/538/p29.pdf?sequence=1&isAllowed=y</a>
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Universal Decimal Classification
Koha item type Journal article

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