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Volumn 414, Issue , 2000, Pages 1-33

Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER; SUPERSONIC FLOW; TURBULENCE;

EID: 0033859289     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112000008466     Document Type: Article
Times cited : (308)

References (48)
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