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The flying hot wire and related instrumentationA flying hot-wire technique is proposed for studies of separated turbulent flow in wind tunnels. The technique avoids the problem of signal rectification in regions of high turbulence level by moving the probe rapidly through the flow on the end of a rotating arm. New problems which arise include control of effects of torque variation on rotor speed, avoidance of interference from the wake of the moving arms, and synchronization of data acquisition with rotation. Solutions for these problems are described. The self-calibrating feature of the technique is illustrated by a sample X-array calibration.
Document ID
19790003181
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Coles, D.
(California Inst. of Tech. Pasadena, CA, United States)
Cantnell, B.
(California Inst. of Tech. Pasadena, CA, United States)
Wadcock, A.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3066
Report Number: NASA-CR-3066
Accession Number
79N11352
Funding Number(s)
CONTRACT_GRANT: NGL-05-002-229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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