A procedure for obtaining velocity vector from two high response impact pressure probes

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procedureforobta00adle.pdf (2.22 MB)
Authors
Adler, Dan
Taylor, Paul M.
Subjects
Flow Measurements
Compressor Flow Fields
Advisors
Date of Issue
1980-08
Date
1980-08
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
A method for experimentally determining the velocity vector for a point in a fluid, downstream of a rotating turboimpeller, is presented. The technique requires four pressure readings from two semiconductor pressure probes and a synchronization system to collect the data. Reduction of the data to the velocity and direction of the fluid particle is performed by the computer program at the end of this report
Type
Technical Report
Description
URI
https://hdl.handle.net/10945/30097
Series/Report No
Department
Organization
Identifiers
NPS Report Number
NPS67-80-007
Sponsors
The work reported herein was initiated under the support of Naval Air Systems Command, Washington, DC and Office of Naval Research, Arlington, VA and completed at the Technion, Haifa, Israel.
Funder
N00019-79-WR-91115
Format
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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