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Two dimensional airfoil optimisation using CFD in a grid computing environment

Two dimensional airfoil optimisation using CFD in a grid computing environment
Two dimensional airfoil optimisation using CFD in a grid computing environment
In this paper, a two-dimensional airfoil shape optimisation problem is investigated using CFD within a grid computing environment (GCE) implemented in Matlab. The feature-based parametric CAD tool ProEngineer is used for geometry modelling. The industrial level mesh generation tool Gambit and flow solver Fluent are employed as remote services using the Globus Toolkit as the low level API. The objective of the optimisation problem is to minimize the drag-to-lift coefficient ratio for the given operating condition. A Matlab interface to the design exploration system (OPTIONS) is used to obtain solutions for the problem. The adoption of grid technologies not only simplifies the integration of proprietary software, but also makes it possible to harness distributed computational power in a consistent and flexible manner.
354040788X
525-532
Springer Berlin, Heidelberg
Song, Wenbin
390dc209-bfcb-4986-8362-c25b40272307
Keane, Andy
26d7fa33-5415-4910-89d8-fb3620413def
Eres, M.H.
b22e2d66-55c4-46d2-8ec3-46317033de43
Pound, Graeme
08828109-c9a9-4e58-8721-a07156526671
Cox, Simon
0e62aaed-24ad-4a74-b996-f606e40e5c55
Song, Wenbin
390dc209-bfcb-4986-8362-c25b40272307
Keane, Andy
26d7fa33-5415-4910-89d8-fb3620413def
Eres, M.H.
b22e2d66-55c4-46d2-8ec3-46317033de43
Pound, Graeme
08828109-c9a9-4e58-8721-a07156526671
Cox, Simon
0e62aaed-24ad-4a74-b996-f606e40e5c55

Song, Wenbin, Keane, Andy, Eres, M.H., Pound, Graeme and Cox, Simon (2003) Two dimensional airfoil optimisation using CFD in a grid computing environment. In Euro-Par 2003 Parallel Processing: 9th International Euro-Par Conference Klagenfurt, Austria, August 26-29, 2003 Proceedings. vol. 2790, Springer Berlin, Heidelberg. pp. 525-532 . (doi:10.1007/b12024).

Record type: Conference or Workshop Item (Paper)

Abstract

In this paper, a two-dimensional airfoil shape optimisation problem is investigated using CFD within a grid computing environment (GCE) implemented in Matlab. The feature-based parametric CAD tool ProEngineer is used for geometry modelling. The industrial level mesh generation tool Gambit and flow solver Fluent are employed as remote services using the Globus Toolkit as the low level API. The objective of the optimisation problem is to minimize the drag-to-lift coefficient ratio for the given operating condition. A Matlab interface to the design exploration system (OPTIONS) is used to obtain solutions for the problem. The adoption of grid technologies not only simplifies the integration of proprietary software, but also makes it possible to harness distributed computational power in a consistent and flexible manner.

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More information

Published date: 2003
Additional Information: within Topic 7: Applications on High-Performance Computers
Venue - Dates: Euro-Par 2003: International Conference on Parallel and Distributed Computing, Klagenfurt, Austria, 2003-08-26 - 2003-08-29
Organisations: Engineering Sciences

Identifiers

Local EPrints ID: 22473
URI: http://eprints.soton.ac.uk/id/eprint/22473
ISBN: 354040788X
PURE UUID: 5a03a5a8-951e-45f2-b147-df70ec980eaf
ORCID for Andy Keane: ORCID iD orcid.org/0000-0001-7993-1569
ORCID for M.H. Eres: ORCID iD orcid.org/0000-0003-4967-0833

Catalogue record

Date deposited: 27 Mar 2006
Last modified: 16 Mar 2024 03:30

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Contributors

Author: Wenbin Song
Author: Andy Keane ORCID iD
Author: M.H. Eres ORCID iD
Author: Graeme Pound
Author: Simon Cox

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