Parallel finite element computation of missile aerodynamics

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1097-0363(199706)24:12<1417::AID-FLD567>3.0.CO;2-N" /><1417::AID-FLD567>3.0.CO;2-N 10.1002/(SICI)1097-0363(199706)24:12<1417::AID-FLD567>3.0.CO;2-NzbMATH Open0882.76047OpenAlexW1994346680MaRDI QIDQ4345495

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Publication date: 5 March 1998

Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(199706)24:12<1417::aid-fld567>3.0.co;2-n

zbMATH Keywords

Navier-Stokes equationsseparated flowlarge Reynolds numbersturbulence modellinghigh angles of attackCRAY T3DThinking Machines CM-5supersonic speedsmultiprocessor mainframes

Mathematics Subject Classification ID

Finite element methods applied to problems in fluid mechanics (76M10) Parallel numerical computation (65Y05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (4)

Finite element methodology for modeling aircraft aerodynamics: development, simulation, and validation ⋮ Fluid–structure interaction modeling with nonmatching interface discretizations for compressible flow problems: Computational framework and validation study ⋮ Stabilized methods for high-speed compressible flows: toward hypersonic simulations ⋮ MIRACLE – a joint DLR/ONERA effort on harmonization and development of industrial and research aerodynamic computational environment

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