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Calibration of a Hot Wire Probe and turbulence measurements

Mercier, T. (2003) Calibration of a Hot Wire Probe and turbulence measurements. DLR-Interner Bericht. 225-2003 A 01, 35 S.

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A hot wire probe was calibrated within the Mach number range from Ma = 0,2 to Ma = 0,95 making use of the DLR wind tunnel SEG in Göttingen. A Dantec single wire probe was oriented at different angles to the flow direction (-30°, -20°, -10°, 0°, 10°, 20°, 30°). Additionally, the probe itself was mounted horizontally as well as vertically to the axis of the calibration jet. Finally, the total pressure was varied (50kPa, 100kPa and 150kPa).

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Calibration of a Hot Wire Probe and turbulence measurements
AuthorsInstitution or Email of Authors
Number of Pages:35
Keywords:hot wire probe, calibration, constant temperature anemometry, turbulence measurements
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L TT - Triebwerkstechnologien
DLR - Research theme (Project):L - Turbine Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:20

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