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Time-sequenced and spectrally filtered Rayleigh imaging of shock wave and boundary layer structure for inlet characterizationMultiple pulsed Rayleigh imaging and filtered Rayleigh scattering are used to generate images of a complex boundary layer structure, shock wave/boundary layer interactions, and crossing shock waves. Time-sequenced Rayleigh images taken with a visible, double-pulsed laser system show the evolution of boundary layer structure of the internal flow in a generic cross-shock inlet. The images taken in the inlet give insight into 3D effects caused by the inlet geometry and may be used for modeling the complex flows.
Document ID
19930066088
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Forkey, Joseph
(NASA Lewis Research Center Cleveland, OH, United States)
Cogne, Sandrine
(NASA Lewis Research Center Cleveland, OH, United States)
Smits, Alexander
(NASA Lewis Research Center Cleveland, OH, United States)
Bogdonoff, Seymour
(NASA Lewis Research Center Cleveland, OH, United States)
Lempert, Walter R.
(NASA Lewis Research Center Cleveland, OH, United States)
Miles, Richard B.
(Princeton Univ. NJ, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 93-2300
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASME, ASEE, AIAA, SAE
Accession Number
93A50085
Distribution Limits
Public
Copyright
Other

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