Reynolds number effects on the prediction of mean flow data for adiabatic 2-D compressible boundary layers

Aeronautical Journal

Volumn 100, Issue 992, 1996, Pages 53-59

  Motallebi, F ^a,b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b UNIVERSITY OF TEHRAN   (Iran)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIBLE FLOW; CONVERGENCE OF NUMERICAL METHODS; CORRELATION METHODS; FRICTION; MATHEMATICAL MODELS; NUMERICAL METHODS; PRESSURE EFFECTS; REYNOLDS NUMBER; SUPERSONIC FLOW; TRANSONIC FLOW; VELOCITY;

ADIABATIC CONDITIONS; MEAN FLOW DATA; SKIN FRICTION COEFFICIENT; VAN DRIEST MODEL; ZERO PRESSURE GRADIENT;

BOUNDARY LAYERS;

EID: 0030082522     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (25)

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