Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids

DOI10.1016/S0045-7930(00)00033-5zbMath1057.76042OpenAlexW2087955052MaRDI QIDQ5942607

Yasushi Ito, Kazuhiro Nakahashi, Fumiya Togashi, Yuichi Shimbo, Toshiyuki Iwamiya

Publication date: 2001

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(00)00033-5

zbMATH Keywords

moving gridChimera method

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Supersonic flows (76J20)

Related Items (4)

Applications of dynamic hybrid grid method for three-dimensional moving/deforming boundary problems ⋮ Aeronautical CFD in the age of petaflops-scale computing: from unstructured to Cartesian meshes ⋮ A dynamic mesh strategy applied to the simulation of flapping wings ⋮ Three-dimensional automatic local remeshing for two or more hybrid meshes

Cites Work

• Implicit Schemes and LU Decompositions

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