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A method of calibrating wind velocity sensors with a modified gas flow calibratorA procedure was described for calibrating air velocity sensors in the exhaust flow of a gas flow calibrator. The average velocity in the test section located at the calibrator exhaust was verified from the mass flow rate accurately measured by the calibrator's precision sonic nozzles. Air at elevated pressures flowed through a series of screens, diameter changes, and flow straighteners, resulting in a smooth flow through the open test section. The modified system generated air velocities of 2 to 90 meters per second with an uncertainty of about two percent for speeds below 15 meters per second and four percent for the higher speeds. Wind tunnel data correlated well with that taken in the flow calibrator.
Document ID
19780013483
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stump, H. P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-78707
Report Number: NASA-TM-78707
Accession Number
78N21426
Funding Number(s)
PROJECT: RTOP 992-19-00-18
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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