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A numerical investigation of supersonic nozzle boundary layer transition
Laura L. Pauley
, Samir N. Dagher
Mechanical Engineering
Research output
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peer-review
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Dive into the research topics of 'A numerical investigation of supersonic nozzle boundary layer transition'. Together they form a unique fingerprint.
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Keyphrases
Area Ratio
20%
Boundary Layer
20%
Boundary Layer Transition
100%
Chamber Pressure
40%
Disturbance Structures
20%
Görtler Vortices
20%
Laminar Boundary Layer
80%
Nozzle
100%
Numerical Investigation
100%
Operating Conditions
20%
Stability Analysis
60%
Supersonic Nozzle
100%
Transition Onset
20%
Turbulent Boundary Layers
20%
Vortex
20%
Wall Heat Flux
60%
Engineering
Area Ratio
25%
Boundary Layer
25%
Boundary Layer Transition
100%
Chamber Pressure
50%
Laminar Boundary Layer
100%
NASA
25%
Stability Analysis
75%
Turbulent Boundary Layer
25%
Vortex
50%
Earth and Planetary Sciences
Boundary Layer
25%
Laminar Boundary Layer
100%
Pressure Chamber
50%
Stability Analysis
75%
Turbulent Boundary Layer
25%
Physics
Boundary Layer
33%
Boundary Layer Transition
100%
Supersonics
100%
Turbulent Boundary Layer
33%