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Active Thermal Isolation For Hot-Film AnemometersLocal heating compensates for conduction of heat from sensors into modules. Two hot-film sensors stacked on wind-tunnel model. Outer sensor detects changes in boundary-layer flow. Inner sensor provides active thermal isolation between outer sensor and model. Thermal boundary condition controlled at response time of detection hot-film sensor, significantly less than response time of internally heated model. Requires less power to maintain outer hot-film sensor at given temperature, enabling system to respond over greater dynamic range before power limits of instrument reached. Stacked sensors bonded to surface of most wind-tunnel models, even to curved surfaces, and removed after completion of experiments.
Document ID
19930000454
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Martinson, Scott D.
(NASA Langley Research Center, Hampton, VA.)
Gray, David L.
(NASA Langley Research Center, Hampton, VA.)
Carraway, Debra L.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 16, 2013
Publication Date
August 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 8
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
LAR-14612
Accession Number
93B10454
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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