Effect of grid resolution on accuracy of skin friction and heat transfer in turbulent boundary layers

38th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2000, Pages

  Thivet, Frédéric ^a   Besbes, Omar ^b,c,d   Knight, Doyle D ^b  

^a ONERA   (France)

^b RUTGERS UNIVERSITY   (United States)

^c ECOLE POLYTECHNIQUE   (France)

^d STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ALGEBRA; BOUNDARY LAYER FLOW; FRICTION; HEAT TRANSFER; MESH GENERATION; PLATES (STRUCTURAL COMPONENTS); SKIN FRICTION; TURBULENCE MODELS; TURBULENT FLOW;

ALGEBRAIC MODELING; COMPRESSIBLE BOUNDARY LAYERS; FLAT PLATE BOUNDARY LAYERS; NUMERICAL SOLUTION; QUANTITATIVE RESULT; SKIN FRICTION COEFFICIENT; TURBULENT BOUNDARY LAYERS; TWO-EQUATION MODEL;

BOUNDARY LAYERS;

EID: 85085402765     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-820     Document Type: Conference Paper

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