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A technique to measure a high frequency, repetitively pulsating flow field is presented. Two impact tube probes and a Kiel probe, all with pressure transducers mounted in thier tips are used. Five readings are required to identify a velocity vector at a point. In this report the technique, the numerical procedure and the computer program used are described.
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Mathematical models, Turbomachines, Fluid dynamics, Pressure, MeasurementEdition | Availability |
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A general procedure for obtaining velocity vector from a system of high response impact pressure probes
1979, Naval Postgraduate School
in English
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Edition Notes
"NPS-67-79-007"--Cover.
"July 1979"--Cover.
Title from cover.
"Prepared for: Naval Air Systems Command, Washington, DC and Office of Naval Research, Arlington, VA."
Includes bibliographical references (p. 54).
"Approved for public release; distribution is unlimited"--Cover.
Technical report; 1979.
ck/ 6/2/09.
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