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High-speed laser anemometry based on spectrally resolved Rayleigh scatteringLaser anemometry in unseeded flows based on the measurement of the spectrum of Rayleigh scattered laser light is reviewed. The use of molecular scattering avoids the well known problems (particle lag, biasing effects, seed generation, seed injection) of seeded flows. The fundamental limits on velocity measurement accuracy are determined using maximum likelihood methods. Measurement of the Rayleigh spectrum with scanning Fabry-Perot interferometers is analyzed and accuracy limits are established for both single pass and multipass configurations. Multipass configurations have much higher selectivity and are needed for measurements where there is a large amount of excess noise caused by stray laser light. It is shown that Rayleigh scattering is particularly useful for supersonic and hypersonic flows. The results of the analysis are compared with measurements obtained with a Rayleigh scattering diagnostic developed for study of the exhaust plume of a small hydrogen-oxygen rocket, where the velocities are in the range of 1000 to 5000 m/sec.
Document ID
19910018207
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seasholtz, Richard G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.15:104522
E-6395
NASA-TM-104522
Report Number: NAS 1.15:104522
Report Number: E-6395
Report Number: NASA-TM-104522
Meeting Information
Meeting: International Conference on Laser Anemometry
Location: Cleveland, OH
Country: United States
Start Date: August 5, 1991
End Date: August 9, 1991
Sponsors: Ohio Aerospace Institute, Cleveland State Univ., ASME, European Association for Laser Anemometry, Case Western Reserve Univ.
Accession Number
91N27521
Funding Number(s)
PROJECT: RTOP 505-62-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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