Calibration and application of a combination temperature-pneumatic probe for velocity and rotor loss distribution measurements in a compressor

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Author
Nuehoff, F.
Date
1981-12
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Abstract
A description is given of the current design of a temperaturepneumatic probe used for radial flow field surveys in an axial compressor. The procedure used to calibrate the probe for variations in Mach number, pitch and yaw angles in a free jet is described and the procedure for representing the characteristics of the probe analytically as three polynomial surfaces, is given.
Description
Interim Report. Principal Investigator, Dr. R. P. Shreeve, Director, Turbopropulsion Laboratory, Naval Postgraduate School, Monterey, California, 93940
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.
URI
http://hdl.handle.net/10945/29207
NPS Report Number
NPS67-81-03CR
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