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Calibration of seven-hole pressure probes for use in fluid flows with large angularityDescribed here is the calibration of a non-nulling, conical, seven-hole pressure probe over a large range of flow onset angles. The calibration procedure is based on the use of differential pressures to determine the three components of velocity. The method allows determination of the flow angle to within 0.5 deg and velocity magnitude to approximately 1.0 percent. Also included is an examination of the factors which limit the use of the probe, a description of the measurement chain, an error analysis, and a typical experimental result. In addition, a new general analytical model of pressure probe behavior is described and the validity of the model is demonstrated by comparing it with experimentally measured calibration data for a three-hole yaw meter and a seven-hole probe.
Document ID
19900006083
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Zilliac, Gregory G.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1989
Subject Category
Instrumentation And Photography
Report/Patent Number
A-89163
NASA-TM-102200
NAS 1.15:102200
Report Number: A-89163
Report Number: NASA-TM-102200
Report Number: NAS 1.15:102200
Accession Number
90N15399
Funding Number(s)
PROJECT: RTOP 505-61-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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