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Quantitative visualization of supersonic flow using Rayleigh scattering
J. Poggie, Alexander Smits
Mechanical & Aerospace Engineering
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Dive into the research topics of 'Quantitative visualization of supersonic flow using Rayleigh scattering'. Together they form a unique fingerprint.
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Keyphrases
Supersonic Flow
100%
Rayleigh Scattering
100%
Quantitative Visualization
100%
Turbulent Mixing Layer
50%
Nanometer Scale
50%
Mach number
50%
Mixing Layer Flow
50%
Probe Measurement
50%
Scattering Particles
50%
Turbulent Structure
50%
Turbulent Boundary Layer Flow
50%
Physical Features
50%
Flow Visualization Technique
50%
Scale Direction
50%
Contaminant Particles
50%
Engineering
Layer Flow
100%
Supersonic Flow
100%
Mixing Layer
50%
Nanometre
50%
Turbulent Boundary Layer
50%
Mach Number
50%
Flow Visualization
50%
Probe Point
50%
Material Science
Supersonic Flow
100%
Computer Science
Visualization Technique
100%