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Research sensorsThe LeRC program in research sensors is directed at development of sensors and sensing techniques for research applications on turbine engines and propulsion systems. In general, the sensors are used either to measure to response of an engine component to the imposed environment. Locations of concern are generally within the gas path and, for the most part, are within the hot section of the engine. Since these sensors are used for research testing as opposed to operational use, a sensor lifetime of the order of 50 hr is considered sufficient. The following discussion presents a sample of this work, describing programs to develop a dynamic gas temperature measuring system, total heat flux sensors, a variety of thin-film sensors, and high-temperature strain measuring systems.
Document ID
19920013283
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Englund, David R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1990
Publication Information
Publication: Aeropropulsion 1987
Subject Category
Instrumentation And Photography
Accession Number
92N22526
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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