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The 16-foot transonic tunnel laser velocimeter systemThe Langley 16-foot transonic wind tunnel is described. The system configuration, optical layout, laser color separator, optical receiver, and tunnel window are discussed.
Document ID
19820024815
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Franke, J. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1982
Publication Information
Publication: Flow Visualization and Laser Velocimetry for Wind Tunnels
Subject Category
Instrumentation And Photography
Accession Number
82N32691
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820024787Collected WorksFlow Visualization and Laser Velocimetry for Wind Tunnels19820024787Collected WorksFlow Visualization and Laser Velocimetry for Wind Tunnels
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