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Variable turbulent Prandtl number model applied to hypersonic shock/boundary-layer interactions
Variable turbulent Prandtl number model applied to hypersonic shock/boundary-layer interactions
2018
Subhajit Roy
Krishnendu Sinha
Keywords:
Hypersonic speed
Geophysics
Boundary layer
Turbulent Prandtl number
Physics
Mechanics
Correction
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