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Accuracy Of Hot-Wire Anemometry In Supersonic TurbulenceSensitivity of hot-wire probe compared to laser-induced-florescence measurements. Report discusses factors affecting readings of hot-wire anemometer in turbulent supersonic boundary layer. Presents theoretical analysis of responses of hot-wire probe to changes in flow; also compares measurements by hot-wire probe with measurements of same flows by laser-induced fluorescence (LIF). Because LIF provides spatially and temporally resolved data on temperature, density, and pressure, provides independent means to determine responses of hot-wire anemometers to these quantities.
Document ID
19890000295
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Logan, Pamela
(NASA Ames Research Center, Moffett Field, CA.)
Mckenzie, Robert L.
(NASA Ames Research Center, Moffett Field, CA.)
Bershader, Daniel
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
June 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 6
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
ARC-11802
Accession Number
89B10295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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