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DNS of boundary layer transition at Mach 6

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3D direct numerical simulation is employed for studying the flat-plate boundary layer instability evolving at high free- stream Mach number to study the non-linear interactions of the disturbances of different modes and the onset of the transition to turbulence.

Author(s):

Dmitry Khotyanovsky    
Institute of Theoretical and Applied Mechanics
Russian Federation

Alexey Kudryavtsev    
Institute of Theoretical and Applied Mechanics
Russian Federation