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A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnelA three-component dual-beam laser-velocimeter system has been designed, fabricated, and implemented in the 7-by 10-Foot Wind Tunnel at NASA Ames Research Center. The instrument utilizes optical access from both sides and the top of the test section, and is configured for uncoupled orthogonal measurements of the three Cartesian coordinates of velocity. Bragg cell optics are used to provide fringe velocity bias. Modular system design provides great flexibility in the location of sending and receiving optics to adapt to specific experimental requirements. Near-focus Schmidt-Cassegrain optic modules may be positioned for collection of forward or backward scattered light over a large solid angle, and may be clustered to further increase collection solid angle. Multimode fiber optics transmit collected light to the photomultiplier tubes for processing. Counters are used to process the photomultiplier signals and transfer the processed data digitally via buffered interface controller to the host MS-DOS computer. Considerable data reduction and graphical display programming permit on-line control of data acquisition and evaluation of the incoming data. This paper describes this system in detail and presents sample data illustrating the system's capability.
Document ID
19950014906
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dunagan, Stephen E.
(NASA Ames Research Center Moffett Field, CA, United States)
Cooper, Donald L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1995
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.15:108864
A-95032
NASA-TM-108864
Accession Number
95N21323
Funding Number(s)
PROJECT: RTOP 505-59-54
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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