Direct numerical simulation of discrete roughness on a swept-wing leading edge

AIAA Journal

Volumn 48, Issue 11, 2010, Pages 2660-2673

  Rizzetta, Donald P ^a   Visbal, Miguel R ^a   Reed, Helen L ^b,c   Saric, William S ^b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b TEXAS A AND M UNIVERSITY   (United States)

^c RBAC ^*  (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

CROSS-FLOW INSTABILITIES; CROSSFLOW VORTICES; DIRECT SIMULATION; DOMAIN DECOMPOSITIONS; FLOW CONDITION; GEOMETRIC ROUGHNESS; HIGH FIDELITY; HIGH-ORDER; LEADING EDGE; LOW-PASS; MESH SYSTEM; PARABOLIC CYLINDER; PARABOLIZED STABILITY EQUATIONS; PARALLEL COMPUTING PLATFORM; REGION OF INTEREST; ROUGHNESS ELEMENTS; SIZE AND SHAPE; SPATIAL ACCURACY; STABILITY CALCULATION; TIME-IMPLICIT;

DELTA WING AIRCRAFT; DIRECT NUMERICAL SIMULATION; DOMAIN DECOMPOSITION METHODS; GEOMETRY; LOW PASS FILTERS; MATHEMATICAL OPERATORS; NONLINEAR EQUATIONS; NUMERICAL METHODS; PARALLEL ARCHITECTURES; REYNOLDS NUMBER; STABILITY; SWEPT WINGS; VORTEX FLOW;

FLOW SIMULATION;

EID: 78649516829     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050548     Document Type: Conference Paper

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