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Constant-temperature hot-wire anemometer practice in supersonic flows. I - The normal wireThe performance of a constant-temperature normal hot-wire in a supersonic flow is critically examined. It is shown that this instrument is inherently unsuitable for measuring turbulent temperature correlations because of the highly nonlinear response to temperature fluctuations, particularly at low overheat ratios. The instrument is therefore limited to measurements of mean and fluctuating mass-flow rates. Suitable calibration procedures, as well as the limits on spatial and temporal resolution are discussed, and corrections for mean stagnation temperature changes are suggested.
Document ID
19830035267
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smits, A. J.
(Princeton Univ. NJ, United States)
Hayakawa, K.
(Princeton Univ. NJ, United States)
Muck, K. C.
(Princeton University Princeton, NJ, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 83-0050
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16485
Funding Number(s)
CONTRACT_GRANT: NAGW-240
Distribution Limits
Public
Copyright
Other

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