Aerodynamic computations using the convective-upstream split-pressure scheme with local preconditioning

AIAA journal

Volumn 38, Issue 3, 2000, Pages 402-410

  Nemec, M ^a   Zingg, D W ^a  

^a UNIVERSITY OF TORONTO   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; BOUNDARY LAYER FLOW; CONVERGENCE OF NUMERICAL METHODS; SHOCK WAVES; SUBSONIC FLOW; TRANSONIC FLOW; TURBULENT FLOW;

CONVECTIVE UPSTREAM SPLIT PRESSURE (CUSP) METHOD; MACH NUMBER;

AERODYNAMICS;

EID: 0033894317     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.998     Document Type: Article

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