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Listening to Turbulence: Measuring Coherence Decay at Different Positions on an Aircraft in Cruise Flight

Haxter, Stefan and Spehr, Carsten (2015) Listening to Turbulence: Measuring Coherence Decay at Different Positions on an Aircraft in Cruise Flight. Journal of Sound and Vibration, 357 (11), pp. 107-127. Elsevier. DOI: 10.1016/j.jsv.2015.07.005 ISSN 0022-460X

Full text not available from this repository.

Official URL: http://www.sciencedirect.com/science/journal/0022460X

Abstract

Measurements of the coherence length were conducted using a pressure transducer array at three different positions on an Airbus Model A320 aircraft. The measured coherence lengths were compared to values predicted by the model of Efimtsov. The predicted values were found considerably lower than the measured values.

Item URL in elib:https://elib.dlr.de/95955/
Document Type:Article
Additional Information:Artikel, p. 117, http://dx.doi.org/10.1016/j.jsv.2015.07.005, http://dx.doi.org/10.1016/j.jsv.2015.07.005, Available online 6 August 2015
Title:Listening to Turbulence: Measuring Coherence Decay at Different Positions on an Aircraft in Cruise Flight
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Haxter, StefanStefan.Haxter (at) dlr.deUNSPECIFIED
Spehr, CarstenCarsten.Spehr (at) dlr.deUNSPECIFIED
Date:2015
Journal or Publication Title:Journal of Sound and Vibration
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:357
DOI :10.1016/j.jsv.2015.07.005
Page Range:pp. 107-127
Publisher:Elsevier
Series Name:Aeroacoustics research in Europe: The CEAS-ASC report on 2014 highlights
ISSN:0022-460X
Status:Published
Keywords:coherence decay, position on aircraft, in-flight
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:29 Sep 2015 14:46
Last Modified:10 Jan 2019 15:49

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