Modified spalart-allmaras one-equation turbulence model for rough wall boundary layers

Journal of Propulsion and Power

Volumn 12, Issue 4, 1996, Pages 809-812

  Lee, Jaesoo ^a,b,c   Paynter, Gerald C ^a,b,c  

^a BOEING COMPANY   (United States)

^b M S 49 53

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC PROPERTIES; BOUNDARY CONDITIONS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; MATHEMATICAL MODELS; PRESSURE EFFECTS; SURFACE ROUGHNESS; TURBULENCE; TURBULENT FLOW; VELOCITY; VISCOSITY;

ACOUSTIC LINING MATERIALS; ACOUSTICALLY TREATED SURFACES; KINEMATIC EDDY VISCOSITY; KINEMATIC MOLECULAR VISCOSITY; MOMENTUM THICKNESS; PRESSURE GRADIENT; SPALART-ALLMARAS ONE EQUATION TURBULENCE MODEL; TRIDIAGONAL MATRIX;

AERODYNAMICS;

EID: 0030190336     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/3.24106     Document Type: Article

References (11)

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