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Coherent anti-Stokes Raman Scattering for Determining Key Thermodynamic Properties of Supersonic, Combusting, and Nonequilibrium Flows
Document ID
20205011163
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Chloe E. Dedic (University of Virginia Charlottesville, Virginia, United States)
Date Acquired
December 7, 2020
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: December 2020 Joint Army-Navy-NASA-Air Force (JANNAF) Meeting
Location: Virtual
Country: US
Start Date: December 7, 2020
End Date: December 17, 2020
Sponsors: Joint Army-Navy-NASA-Air Force (JANNAF)
Funding Number(s)
WBS: 394364.04.25.23.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
CARS
Coherent anti-Stokes Raman Scattering
laser based measurement,
hypersonic
plume flow
wake flow

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