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Instrumentation for propulsion systems developmentApparatus and techniques developed or used by NASA-Lewis to make steady state or dynamic measurements of gas temperature, pressure, and velocity and of the temperature, tip clearance, and vibration of the blades of high-speed fans or turbines are described. The advantages and limitations of each instrument and technique are discussed and the possibility of modifying them for use in developing various propulsion systems is suggested.
Document ID
19780009109
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Warshawsky, I. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-73840
Report Number: NASA-TM-73840
Meeting Information
Meeting: Soc. of Automotive Engr. Congr. (Meeting 1M21)
Location: Detroit
Start Date: February 27, 1978
End Date: March 3, 1978
Accession Number
78N17052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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