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Progress on a Rayleigh Scattering Mass Flux Measurement TechniqueA Rayleigh scattering diagnostic has been developed to provide mass flux measurements in wind tunnel flows. Spectroscopic molecular Rayleigh scattering is an established flow diagnostic tool that has the ability to provide simultaneous density and velocity measurements in gaseous flows. Rayleigh scattered light from a focused 10 Watt continuous-wave laser beam is collected and fiber-optically transmitted to a solid Fabry-Perot etalon for spectral analysis. The circular interference pattern that contains the spectral information that is needed to determine the flow properties is imaged onto a CCD detector. Baseline measurements of density and velocity in the test section of the 15 cm x 15 cm Supersonic Wind Tunnel at NASA Glenn Research Center are presented as well as velocity measurements within a supersonic combustion ramjet engine isolator model installed in the tunnel test section.
Document ID
20110016051
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Mielke-Fagan, Amy F.
(NASA Glenn Research Center Cleveland, OH, United States)
Clem, Michelle M.
(NASA Glenn Research Center Cleveland, OH, United States)
Elam, Kristie A.
(Jacobs Sverdrup Technology, Inc. United States)
Hirt, Stefanie M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2010
Subject Category
Aerodynamics
Report/Patent Number
AIAA-Paper-2010-856
E-17951
Meeting Information
Meeting: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Location: Orlando, FL
Country: United States
Start Date: January 4, 2010
End Date: January 7, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 599489.02.07.03.03.12.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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