The effect of numerical dissipation on high reynolds number turbulent flow solutions

34th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1996, Pages

  McNeil, C Y ^a  

^a BAE SYSTEMS   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; BUDGET CONTROL; COST EFFECTIVENESS; PRODUCT DESIGN; REYNOLDS NUMBER; TURBULENT FLOW;

BOUNDARY LAYER THICKNESS; CENTRAL DIFFERENCE SCHEME; GRID CONVERGENCE; HIGH REYNOLDS NUMBER; MOMENTUM BUDGET; NUMERICAL DISSIPATION; SCALAR DISSIPATION; STRUCTURED GRID;

ATMOSPHERIC THERMODYNAMICS;

EID: 85086950726     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-891     Document Type: Conference Paper

References (19)

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