Computational study of a supersonic base flow using LES/RANS hybrid methodology

AIAA Paper

Volumn , Issue , 2004, Pages 4075-4085

  Kawai, Soshi ^a   Fujii, Kozo ^b  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FLOW MEASUREMENT; KINEMATICS; MOLECULAR DYNAMICS; NAVIER STOKES EQUATIONS; PRESSURE EFFECTS; REYNOLDS NUMBER; ROBUSTNESS (CONTROL SYSTEMS); SPECIFIC HEAT; STRAIN RATE; TENSORS; UNSTEADY FLOW; VISCOSITY;

CARTESIAN COORDINATES; FREESTREAM VELOCITY; LARGE EDDY SIMULATIONS (LES); MACH NUMBER;

SUPERSONIC FLOW;

EID: 2942729591     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-68     Document Type: Conference Paper

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