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New developments in understanding supersonic turbulent boundary layers
A. J. Smits
Mechanical & Aerospace Engineering
Research output
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Contribution to conference
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Paper
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peer-review
5
Scopus citations
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Dive into the research topics of 'New developments in understanding supersonic turbulent boundary layers'. Together they form a unique fingerprint.
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Keyphrases
Physical Mechanism
100%
Mach number
100%
Turbulent Boundary Layers
100%
Reynolds number Dependence
100%
Supersonic Turbulent Boundary Layer
100%
Supersonic Flow
100%
Large-scale Motions
100%
Compressible Boundary Layers
100%
Incompressible Boundary Layer
100%
Physics
Supersonics
100%
Turbulent Boundary Layer
100%
Mach Number
50%
Reynolds Number
50%
Supersonic Flow
50%
Compressible Boundary Layer
50%
Incompressible Boundary Layer
50%
Engineering
Turbulent Boundary Layer
100%
Boundary Layer
50%
Reynolds' Number
50%
Simple Model
50%
Supersonic Flow
50%
Scale Motion
50%