Supersonic base-flow computation using higher-order closure turbulence models

Journal of Spacecraft and Rockets

Volumn 33, Issue 3, 1996, Pages 374-380

  Chuang, C C ^a   Chieng, C C ^b,c  

^a CHUNG SHAN INSTITUTE OF SCIENCE AND TECHNOLOGY   (Taiwan)

^b NATIONAL TSING HUA UNIVERSITY   (Taiwan)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRA; ALGORITHMS; CONVERGENCE OF NUMERICAL METHODS; MATHEMATICAL MODELS; MISSILES; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; REYNOLDS NUMBER; SUPERSONIC FLOW; TURBULENCE;

BI-CONJUGATE GRADIENT TABLE SCHEME; HIGHER ORDER CLOSURE TURBULENCE MODELS; RECOMPRESSION REGION; REYNOLDS STRESS MODEL; SUPERSONIC BASE FLOW COMPUTATION; TWO EQUATION MODEL; TWO LAYER ALGEBRAIC STRESS MODEL; TWO STREAM FLOW;

COMPUTATIONAL FLUID DYNAMICS;

EID: 0030147699     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/3.26770     Document Type: Article

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