Comparison of unstructured grid finite volume methods for cold gas hypersonic flow simulations

16th AIAA Applied Aerodynamics Conference

Volumn , Issue , 1998, Pages 447-463

  Azevedo, Joảo Luiz F ^a   Korzenowski, Heidi ^b  

^a INSTITUTO DE AERONÁUTICA E ESPAÇO   (Brazil)

^b INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FINITE VOLUME METHOD; FLOW OF GASES; HYPERSONIC INLETS; MESH GENERATION;

ADAPTIVE MESH REFINEMENT; ADAPTIVE REFINEMENT STRATEGY; CENTRAL DIFFERENCE; COMPARATIVE PERFORMANCE; FLUX VECTOR SPLITTING SCHEMES; SPATIAL DISCRETIZATION SCHEMES; UNSTRUCTURED GRID; UNSTRUCTURED TRIANGULAR MESHES;

HYPERSONIC FLOW;

EID: 84983103153     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2629     Document Type: Conference Paper

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