Exploring the validity of the Spalart-Allmaras turbulence model for hypersonic flows

Journal of Spacecraft and Rockets

Volumn 35, Issue 2, 1998, Pages 121-126

  Paciorri, R ^a,b   Dieudonne W ^a   Degrez, G ^a,c   Charbonnier, J M ^a   Deconinck, H ^a,c  

^a VON KARMAN INSTITUTE FOR FLUID DYNAMICS   (Belgium)

^b SAPIENZA UNIVERSITY OF ROME   (Italy)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; FINITE DIFFERENCE METHOD; FINITE VOLUME METHOD; HEAT TRANSFER; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); TURBULENT FLOW; WIND TUNNELS;

HOLLOW CYLINDER FLARE; MACH NUMBER; SPALART-ALLMARAS TURBULENCE MODEL;

HYPERSONIC FLOW;

EID: 0032021503     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3307     Document Type: Article

References (20)

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