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Hot wire anemometry in transonic flowThe use of hot-wire anemometry for obtaining fluctuating data in transonic flows has been evaluated. From hot-wire heat loss correlations based on previous transonic data, the sensitivity coefficients for velocity, density, and total temperature fluctuations have been calculated for a wide range of test conditions and sensor parameters. For sensor Reynolds numbers greater than 20 and high sensor overheat ratios, the velocity sensitivity remains independent of Mach number and equal to the density sensitivity. These conclusions were verified by comparisons of predicted sensitivities with those from recent direct calibrations in transonic flows. Based on these results, techniques are presented to obtain meaningful measurements of fluctuating velocity, density, and Reynolds shear stress using hot-wire and hot-film anemometers. Examples of these measurements are presented for two transonic boundary layers.
Document ID
19760012280
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Horstman, C. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Rose, W. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-X-62495
A-6309
Accession Number
76N19368
Funding Number(s)
PROJECT: RTOP 505-06-13-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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