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Transonic applications of the Wake Imaging SystemThe extension of a rapid flow field survey method (wake imaging system) originally developed for low speed wind tunnel operation, to transonic wind tunnel applications is discussed. The advantage of the system, beside the simplicity and low cost of the data acquisition system, is that the probe position data are recorded as an optical image of the actual sensor and thus are unaffected by the inevitable deflections of the probe support. This permits traversing systems which are deliberately flexible and have unusual motions. Two transverse drive systems are described and several typical data images are given.
Document ID
19820024800
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crowder, J. P.
(Boeing Co. Seattle, WA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1982
Publication Information
Publication: NASA. Langley Research Center Flow Visualization and Laser Velocimetry for Wind Tunnels
Subject Category
Instrumentation And Photography
Accession Number
82N32676
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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