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Some influences of approximate values for velocity, density and total temperature sensitivities on hot wire anemometer resultsThere is a renewed interest in hot wire anemometry at transonic speeds. Recent results were published which indicate that at transonic speeds a heated wire is sensitive only to mass flow and total temperature, results similar to those obtained for supersonic flows. Other results were obtained to show that the sensitivity is a function of velocity, density, and total temperature, results in agreement with many of those obtained in the 1950s. An analysis of anemometry results was made to evaluate possible errors when various assumptions were made concerning the sensitivity of a heated wire to fluid flow variables.
Document ID
19860035179
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stainback, P. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 86-0506
Accession Number
86A19917
Distribution Limits
Public
Copyright
Other

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