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Microsensor Hot-Film AnemometerImproved hot-film anemometer developed for making high-bandwidth turbulence measurements in moderate-enthalpy supersonic and hypersonic flows (e.g., NASP inlets and control surfaces, HSCT jet exhaust). Features include low thermal inertia, ruggedness, and reduced perturbation of flow.
Document ID
19950065328
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcginley, Catherine B. (NASA Langley Research Center, Hampton, VA.)
Stephens, Ralph (NASA Langley Research Center, Hampton, VA.)
Hopson, Purnell (NASA Langley Research Center, Hampton, VA.)
Bartlett, James E. (NASA Langley Research Center, Hampton, VA.)
Sheplak, Mark (Syracuse Univ.)
Spina, Eric F. (Syracuse Univ.)
Date Acquired
August 17, 2013
Publication Date
April 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 4
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
LAR-15112
Accession Number
95B10169
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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