Mean flowfield scaling of supersonic shock-free three-dimensional turbulent boundary layer

AIAA journal

Volumn 38, Issue 11, 2000, Pages 2120-2126

  Konrad, W ^a,c   Smits, A J ^a   Knight, D ^b  

^a PRINCETON UNIVERSITY   (United States)

^b RUTGERS UNIVERSITY   (United States)

^c BMW AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTER SIMULATION; FLOW VISUALIZATION; FRICTION; NAVIER STOKES EQUATIONS; PRESSURE EFFECTS; TURBULENT FLOW; VISCOSITY;

PITOT PRESSURE; SURFACE SKIN FRICTION; WALL STATIC PRESSURE; YAW ANGLE;

SUPERSONIC FLOW;

EID: 0034322952     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.874     Document Type: Article

References (22)

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