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Subminiature Hot-Wire ProbesClass of improved subminiature hot-wire flow-measuring probes developed. Smaller sizes yield improved resolution in measurements of practical aerodynamic flows. Probe made in one-wire, two-perpendicular-wire, and three-perpendicular-wire version for measurement of one, two, or all three components of flow. Oriented and positioned on micromanipulator stage and viewed under microscope during fabrication. Tested by taking measurements in constant-pressure turbulent boundary layer. New probes give improved measurements of turbulence quantities near surfaces and anisotropies of flows strongly influence relative errors caused by phenomena related to spatial resolution.
Document ID
19890000504
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Westphal, R. V.
(NASA Ames Research Center, Moffett Field, CA.)
Lemos, F. R.
(NASA Ames Research Center, Moffett Field, CA.)
Ligrani, P. M.
(Naval Postgraduate School)
Date Acquired
August 14, 2013
Publication Date
October 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 10
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
ARC-12228
Accession Number
89B10504
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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