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Parallelisation and performance evaluation of the aeronautical CFD flow code ESAUNA

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High-Performance Computing and Networking (HPCN-Europe 1996)

Part of the book series: Lecture Notes in Computer Science ((LNCS,volume 1067))

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Abstract

The parallelisation of an industrially important in-house CFD code for calculating the airflow over complex aircraft configurations using the Euler or Navier-Stokes equations is described. The code uses a novel grid system which may include block-structured hexahedral grids, unstructured tetrahedral grids or a hybrid combination of both. Some details of the parallelisation approach are discussed and performance results for industrial scale test cases running on three parallel platforms: Cray T3D, IBM SP2, Parsytec GC/PP are presented. Some lessons learned during the project are briefly noted.

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References

  1. Childs P N, Shaw J A, Peace A J, Georgala J M, SAUNA — A System for Grid Generation and Flow Simulation using Hybrid Structured/Unstructured Grids, ECCOMAS, Brussels, 1992

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  2. Ierotheou C S, Forsey C R, Block U, Parallelisation of a Novel 3D Hybrid Structured-Unstructured Grid CFD Production Code, HPCN, Milan, 1995

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  3. Walshaw C, JOSTLE: Partitioning of Unstructured Meshes for Massively Parallel Machines, Parallel CFD94, Japan, 1994

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Heather Liddell Adrian Colbrook Bob Hertzberger Peter Sloot

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© 1996 Springer-Verlag Berlin Heidelberg

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Forsey, C.R., Ierotheou, C.S., Block, U., Leatham, M. (1996). Parallelisation and performance evaluation of the aeronautical CFD flow code ESAUNA. In: Liddell, H., Colbrook, A., Hertzberger, B., Sloot, P. (eds) High-Performance Computing and Networking. HPCN-Europe 1996. Lecture Notes in Computer Science, vol 1067. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-61142-8_537

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  • DOI: https://doi.org/10.1007/3-540-61142-8_537

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-61142-4

  • Online ISBN: 978-3-540-49955-8

  • eBook Packages: Springer Book Archive

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