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Acoustic Pressure-Velocity-Probe Calibration using High-Speed PIV

Koop, Lars and Kröber, Stefan and Henning, Arne (2010) Acoustic Pressure-Velocity-Probe Calibration using High-Speed PIV. 15th International Symposium on Application Laser Techniques to Fluid Mechanics, 05. - 08. Juli 2010, Lisbon, Portugal.

Full text not available from this repository.

Official URL: http://ltces.dem.ist.utl.pt/lxlaser/lxlaser2010/

Abstract

In order to calibrate the velocity transducer of a acoustic pressure-velocity-probe, absolute levels of the acoustic particle velocity are obtained in the present investigation by means of particle image velocimetry (PIV) measurements, sampled up to a frequency of 20 kHz. For the frequency distribution of the measured acoustic particle velocity the dynamic range reaches up to 65 dB. It will be shown that the used high-speed PIV system is a very powerful tool to obtain absolute velocity levels in a large frequency range. One big advantage of this measurement technique is that it can be performed in any sound-field and does not depend on a large anechoic room.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Acoustic Pressure-Velocity-Probe Calibration using High-Speed PIV
Authors:
AuthorsInstitution or Email of Authors
Koop, LarsUNSPECIFIED
Kröber, StefanUNSPECIFIED
Henning, ArneTU-Berlin
Date:2010
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-11
Series Name:Conference Proceedings on USB-Stick
Status:Published
Keywords:acoustic pressure-velocity-probe, particle image velocimetry (PIV), High-speed PIV,
Event Title:15th International Symposium on Application Laser Techniques to Fluid Mechanics
Event Location:Lisbon, Portugal
Event Type:international Conference
Event Dates:05. - 08. Juli 2010
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:21 Jul 2010 14:16
Last Modified:21 Jul 2010 14:16

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