The implementation of an aeronautical CFD flow code onto distributed memory parallel systems

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1097-0363(20000430)32:8<903::AID-FLD950>3.0.CO;2-C" /><903::AID-FLD950>3.0.CO;2-C 10.1002/(SICI)1097-0363(20000430)32:8<903::AID-FLD950>3.0.CO;2-CzbMath0980.76050OpenAlexW1994467428MaRDI QIDQ4484666

C. S. Ierotheou, C. R. Forsey, M. Leatham

Publication date: 25 May 2000

Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(20000430)32:8<903::aid-fld950>3.0.co;2-c

zbMATH Keywords

Navier-Stokes equationsconvergence accelerationdomain decompositionEuler equationsparallelizationcomputational fluid dynamics codehybrid gridblock-structured gridsunstructured tetrahedral gridsimplicit residual smoothingcomplex aircraft configurationsdistributed memory parallel systemsencapsulated message passingmultigrid full approximation storage schemeSAUNA CFD suitesingle programme multiple data

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Gas dynamics (general theory) (76N15) Parallel numerical computation (65Y05)

Uses Software

• JOSTLE
• CAPTools
• SAUNA
• Unnamed Item

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