Flow computations around delta wings using unstructured hybrid grids

Journal of Aircraft

Volumn 36, Issue 2, 1999, Pages 374-379

  Kano, Shintaro ^a   Nakahashi, Kazuhiro ^a  

^a TOHOKU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYER FLOW; COMPRESSIBLE FLOW; CONVERGENCE OF NUMERICAL METHODS; DATA REDUCTION; DELTA WING AIRCRAFT; FINITE VOLUME METHOD; INTEGRATION; NAVIER STOKES EQUATIONS; SUBSONIC FLOW; VORTEX FLOW;

GAUSS-SEIDEL IMPLICIT TIME INTEGRATION METHOD; UNSTRUCTURED HYBRID GRIDS;

WINGS;

EID: 0032686480     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2467     Document Type: Article

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