Steinville, R. (2005) Calibration of a three-hole cylindrical pressure probe in sub- and supersonic flow. DLR-Interner Bericht. 225-2005 A 01, 64 S.
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A three-hole cylindrical pressure probe was calibrated within the Mach number range from Ma = 0,3 to Ma = 1,6 making use of the DLR wind tunnel SEG in Göttingen. The probe was oriented at different angles to the flow direction : between -45° and 45° for the pitch angle and between -10° and 10° for the yaw angle . Finally, the total pressure was varied (50kPa, 100kPa).
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Calibration of a three-hole cylindrical pressure probe in sub- and supersonic flow|
|Number of Pages:||64|
|Keywords:||three-hole cylindrical probe, calibration, pressure measurements,|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Propulsion Systems|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Turbine Technologies|
|Institutes and Institutions:||Institute of Propulsion Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 13:35|
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