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DNS of reacting hypersonic turbulent boundary layers
M. Pino Martín
, V. Gregory Weirs
, Debra Olejniczak
,
Graham V Candler
Aerospace Engineering and Mechanics
Research output
:
Contribution to conference
›
Paper
›
peer-review
6
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Scopus citations
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Keyphrases
Direct numerical Simulation
100%
Boundary Layer
100%
Hypersonic Turbulent Boundary Layer
100%
Turbulent Boundary Layers
66%
Shear Stress
66%
Computational Methods
33%
Chemical Reaction
33%
Order of Magnitude
33%
Mach number
33%
Simulation Parameters
33%
Span-wise
33%
Mean Velocity
33%
Temperature Fluctuation
33%
Dilatation
33%
Endothermic Reaction
33%
Comparison with Experimental Results
33%
Velocity Shear
33%
Reynolds Stress
33%
Structure Parameters
33%
Non-reacting
33%
Turbulent Intensity
33%
Supersonic Speed
33%
Supersonic Turbulent Boundary Layer
33%
Numerical Simulation Approach
33%
Physics
Turbulent Boundary Layer
100%
Direct Numerical Simulation
100%
Hypersonics
100%
Boundary Layer
75%
Computational Method
25%
Mach Number
25%
Supersonics
25%
Supersonic Speed
25%
Engineering
Turbulent Boundary Layer
100%
Direct Numerical Simulation
100%
Boundary Layer
75%
Mach Number
25%
Simulation Parameter
25%
Experimental Result
25%
Structure Stress
25%
Temperature Fluctuation
25%
Reynolds Normal Stress
25%
Supersonic Speed
25%
Material Science
Turbulent Boundary Layer
100%
Boundary Layer
75%
Mach Number
25%