Parallelisation and performance evaluation of the aeronautical CFD flow code ESAUNA

  • C R Forsey
  • C S Ierotheou
  • U Block
  • M Leatham
Conference paper
Part of the Lecture Notes in Computer Science book series (LNCS, volume 1067)

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. 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, 1992Google Scholar
  2. 2.
    Ierotheou C S, Forsey C R, Block U, Parallelisation of a Novel 3D Hybrid Structured-Unstructured Grid CFD Production Code, HPCN, Milan, 1995Google Scholar
  3. 3.
    Walshaw C, JOSTLE: Partitioning of Unstructured Meshes for Massively Parallel Machines, Parallel CFD94, Japan, 1994Google Scholar
  4. 4.
    Stanniland D R, in A Selection of Experimental Test Cases for the Validation of CFD Codes, AGARD-AR-303, 1994Google Scholar

Copyright information

© Springer-Verlag 1996

Authors and Affiliations

  • C R Forsey
    • 1
  • C S Ierotheou
    • 2
  • U Block
    • 3
  • M Leatham
    • 4
  1. 1.Aircraft Research Association LtdBedfordUK
  2. 2.Parallel Processing GroupUniversity of GreenwichLondonUK
  3. 3.GENIAS GmbHNeutraublingGermany
  4. 4.Oxford University Computing LaboratoryOxfordUK

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