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Rayleigh Scattering for Measuring Flow in a Nozzle Testing FacilityA molecular Rayleigh-scattering-based air-density measurement system was built in a large nozzle-and-engine-component test facility for surveying supersonic plumes from jet-engine exhaust. A molecular Rayleigh-scattering-based air-density measurement system was built in a large nozzle-and-enginecomponent test facility for surveying supersonic plumes from jet-engine exhaust
Document ID
20100021286
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Tech Brief
External Source(s)
http://www.embeddedtechmag.com/content/view/142/123/
Authors
Gomez, Carlos R. (NASA Glenn Research Center Cleveland, OH, United States)
Panda, Jayanta (Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2006
Publication Information
Publication: NASA Tech Briefs, June 2006
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
LEW-17627-1
Report Number: LEW-17627-1
Distribution Limits
Public
Copyright
Public Use Permitted.

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