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Calibration of a three-hole cylindrical pressure probe in sub- and supersonic flow

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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Abstract

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).

Item URL in elib:https://elib.dlr.de/1302/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Calibration of a three-hole cylindrical pressure probe in sub- and supersonic flow
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Steinville, R.UNSPECIFIEDUNSPECIFIED
Date:2005
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:64
Status:Published
Keywords:three-hole cylindrical probe, calibration, pressure measurements,
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:35

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