Computational study of supersonic base flow using hybrid turbulence methodology

AIAA Journal

Volumn 43, Issue 6, 2005, Pages 1265-1275

  Kawai, Soshi ^a,c   Fujii, Kozo ^b,d  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c JAPAN SOCIETY FOR THE PROMOTION OF SCIENCE   (Japan)

^d JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPRESSIBLE FLOW; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FLOW PATTERNS; NOZZLES; REYNOLDS NUMBER; TURBULENCE;

AEROSPIKE NOZZLES; AXISYMMETRIC BASE FLOW; LARGE EDDIE SIMULATION (LES); MACH NUMBER;

SUPERSONIC FLOW;

EID: 20444462052     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.13690     Document Type: Article

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