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Miniature probes for use in gas turbine testingSeveral examples of miniature probes (null type as well as fixed position) are presented which have proved useful in aircraft and space power systems component testing and are applicable to automotive gas turbine testing. These probes are used to determine component or system performance from the measurement of gas temperature as well as total and static pressure, and flow direction. Detailed drawings of the sensors are presented along with experimental data covering the flow characteristics over the range of intended use.
Document ID
19750006945
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Glawe, G. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Krause, L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-X-71638
Meeting Information
Meeting: Automative Eng. Conf.
Location: Detroit, MI
Country: United States
Start Date: February 24, 1974
End Date: February 28, 1974
Sponsors: Soc. of Automative Engr.
Accession Number
75N15017
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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