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Theoretical derivation and calibration technique of a hemispherical-tipped, five-hole probeA technique is presented for the calibration of a hemispherical tipped 0.125 inch diameter 5-hole probe. The derivation of equations from the potential flow over a sphere relating the flow angle and velocity to pressure differentials measured by the probe is presented. The technique for acquiring the calibration data and the technique used to calculate the calibration coefficients are presented. The accuracy of the probe in both the uniform calibration flow field and the nonuniform flow field over a 75 degree swept delta wing is discussed.
Document ID
19890004025
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kjelgaard, Scott O.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:4047
L-16454
NASA-TM-4047
Accession Number
89N13396
Funding Number(s)
PROJECT: RTOP 505-60-11-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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