Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M = 2.25

Physics of Fluids

Volumn 16, Issue 3, 2004, Pages 530-545

  Pirozzoli, S ^a   Grasso, F ^a   Gatski, T B ^b  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ENERGY DISSIPATION; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SUPERSONIC FLOW; TEMPERATURE DISTRIBUTION; THERMODYNAMICS; TURBULENT FLOW; VELOCITY MEASUREMENT;

ADIABATIC FLAT PLATES; MORKOVIN'S HYPOTHESIS; NONOSCILLATORY COMPACT DIFFERENCE METHOD; TURBULENT BOUNDARY LAYERS;

BOUNDARY LAYER FLOW;

DIRECT NUMERICAL SIMULATION; INCOMPRESSIBLE FLOW; MACH NUMBER; SUPERSONIC FLOW; TURBULENT BOUNDARY LAYER;

EID: 1942443217     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.1637604     Document Type: Article

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