Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number

Journal of Fluid Mechanics

Volumn 672, Issue , 2011, Pages 245-267

  Duan, L ^a   Beekman, I ^a   Martin M P ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

compressible turbulence; high speed flow; turbulent boundary layers

Indexed keywords

AERODYNAMICS; COMPRESSIBILITY; DIRECT NUMERICAL SIMULATION; HYPERSONIC BOUNDARY LAYERS; NUMERICAL MODELS; REYNOLDS NUMBER; TURBULENCE; TURBULENT FLOW;

COMPRESSIBLE TURBULENCE; FREE STREAM MACH NUMBERS; HIGH SPEED FLOWS; LARGE SCALE MOTION; REYNOLDS STRESS TENSORS; THERMODYNAMIC QUANTITIES; TURBULENCE STRUCTURES; TURBULENT BOUNDARY LAYERS;

MACH NUMBER;

EID: 79952090775     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112010005902     Document Type: Article

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