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Rayleigh Scattering Diagnostic for Dynamic Measurement of Velocity Fluctuations in High Speed JetsA flow diagnostic technique based on the molecular Rayleigh scattering of laser light is used to obtain dynamic density and velocity data in a high speed flow. The technique is based on analyzing the Rayleigh scattered light with a Fabry-Perot interferometer used in the static, imaging mode. An analysis is presented that established a lower bound for measurement uncertainty of about 20 m/sec for individual velocity measurements obtained in a 100 microsecond time interval. Software and hardware interfaces were developed to allow computer control of all aspects of the experiment and data acquisition. The signals from three photomultiplier tubes were simultaneously recorded using photon counting at a 10 kHz sampling rate and 10 second recording periods. Density and velocity data, including distribution functions and power spectra, taken in a Mach 0.8 free jet, are presented.
Document ID
20010049425
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Seasholtz, Richard G.
(NASA Glenn Research Center Cleveland, OH United States)
Panda, Jayanta
(Ohio Aerospace Inst. Brook Park, OH United States)
Elam, Kristie A.
(Akima Corp. Fairview Park, OH United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2001
Subject Category
Instrumentation And Photography
Report/Patent Number
E-12739
AIAA Paper 2001-0847
NASA/TM-2001-210821
NAS 1.15:210821
Meeting Information
Meeting: 39th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2001
End Date: January 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 704-20-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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