Supersonic turbulent boundary layer subjected to step changes in wall temperature

AIAA Journal

Volumn 35, Issue 1, 1997, Pages 51-57

  Debiève, Jean François ^a,b   Dupont, Pierre ^a,b   Smith, Douglas R ^a,c,d   Smits, Alexander J ^a,c,e  

^a CNRS   (France)

^b AIX MARSEILLE UNIVERSITÉ   (France)

^c Inst Mecan Statistique Turbulence   (France)

^d Princeton University ^*  (United States)

^e Princeton University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPRESSIBLE FLOW; ENTHALPY; FLOW MEASUREMENT; HEAT TRANSFER COEFFICIENTS; RELAXATION PROCESSES; REYNOLDS NUMBER; SHEAR STRESS; SPECIFIC HEAT OF GASES; THERMAL EFFECTS; TURBULENT FLOW; WALL FLOW;

MACH NUMBER; REYNOLDS STRESS; SKIN FRICTION COEFFICIENT; VON KARMAN CONSTANT;

SUPERSONIC AERODYNAMICS;

EID: 0030784194     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.86     Document Type: Article

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