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A laser-sheet flow visualization technique for the large wind tunnels of the National Full-Scale Aerodynamics ComplexA flow visualization technique for the large wind tunnels of the National Full Scale Aerodynamics Complex (NFAC) is described. The technique uses a laser sheet generated by the NFAC Long Range Laser Velocimeter (LRLV) to illuminate a smoke-like tracer in the flow. The LRLV optical system is modified slightly, and a scanned mirror is added to generate the sheet. These modifications are described, in addition to the results of an initial performance test conducted in the 80- by 120-Foot Wind Tunnel. During this test, flow visualization was performed in the wake region behind a truck as part of a vehicle drag reduction study. The problems encountered during the test are discussed, in addition to the recommended improvements needed to enhance the performance of the technique for future applications.
Document ID
19910000955
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Reinath, M. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Ross, J. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.15:102793
NASA-TM-102793
A-90082
Report Number: NAS 1.15:102793
Report Number: NASA-TM-102793
Report Number: A-90082
Accession Number
91N10268
Funding Number(s)
PROJECT: RTOP 505-61-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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