Turbulence model assessment for shock wave/turbulent boundary-layer interaction in transonic and supersonic flows

Computers and Fluids

Volumn 29, Issue 3, 2000, Pages 275-299

  Liou, William W ^a   Huang, George ^b   Shih, Tsan Hsing ^c  

^a Western Michigan University   (United States)

^b UNIVERSITY OF KENTUCKY   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW; MATHEMATICAL MODEL; REYNOLDS NUMBER; SHOCK WAVE; TURBULENT FLOW;

BOUNDARY LAYER FLOW; COMPUTATIONAL METHODS; MATHEMATICAL MODELS; REYNOLDS NUMBER; SHOCK WAVES; SUPERSONIC FLOW; TRANSONIC FLOW;

CHIEN LOW-REYNOLDS NUMBER MODELS; SHOCK WAVE/TURBULENT BOUNDARY-LAYER INTERACTIONS;

TURBULENT FLOW;

SHOCK WAVE; SUPERSONIC FLOW; TRANSONIC FLOW; TURBULENT BOUNDARY LAYER;

EID: 0034115611     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7930(99)00010-9     Document Type: Article

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