High-order unstructured grid ENO and WENO schemes applied to aerodynamic flows

17th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2005, Pages

  Wolf, William R ^a   Azevedo, João Luiz F ^b  

^a INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

^b INSTITUTO DE AERONÁUTICA E ESPAÇO   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; SHOCK WAVES;

ADAPTIVE MESH REFINEMENT; ESSENTIALLY NON-OSCILLATORY SCHEMES; FLUX DIFFERENCE SPLITTING; FLUX VECTOR SPLITTING; HYPERBOLIC CONSERVATION LAWS; RECONSTRUCTION PROCESS; UNSTRUCTURED MESHES; WEIGHTED ESSENTIALLY NONOSCILLATORY SCHEME;

AERODYNAMICS;

EID: 85086618864     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-5115     Document Type: Conference Paper

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