EPSRC Reference: |
GR/M50539/02 |
Title: |
LARGE EDDY SIMULATION FOR AEROSPACE & TURBOMACHINERY AERODYNAMICS |
Principal Investigator: |
Leschziner, Professor M |
Other Investigators: |
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Researcher Co-Investigators: |
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Project Partners: |
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Department: |
Aeronautics |
Organisation: |
Imperial College London |
Scheme: |
Standard Research (Pre-FEC) |
Starts: |
26 April 2001 |
Ends: |
25 February 2003 |
Value (£): |
6,214
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EPSRC Research Topic Classifications: |
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EPSRC Industrial Sector Classifications: |
Aerospace, Defence and Marine |
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Related Grants: |
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Panel History: |
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Summary on Grant Application Form |
Investigators from UMIST, the University of Surrey, Loughborough University and Imperial College are to embark on a consortium programme to investigate the potential of LES for computing complex engineering flows around aerofoils, blades and combustor guide-vanes. The programme will proceed as a linked set of 4 projects funded by a variety of sponsors. Although the areas of application differ among the projects, all share important common objectives and activities. Common elements include (i) separation from curved surfaces; (ii) the use of body-fitted multi-block FV meshes of relatively low quality; (iii) the fundamental importance of modelling near-wall processes in high-Reflows; (iii) the importance of sub-grid-scale modelling applied in conjunction with skewed and high-aspect-ratio grids; (iv) the search for optimum pressure solvers representing mass conservation; and (v) the search for optimum parallel implementations on HPC97. These issues are to be investigated in a collaborative manner, with information and improved methodologies shared continuously among the partners. The consortium's efforts are to be assisted by Daresbury Laboratory's HPCI Centre.
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Key Findings |
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Potential use in non-academic contexts |
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Impacts |
Description |
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Summary |
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Date Materialised |
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Sectors submitted by the Researcher |
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Project URL: |
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Further Information: |
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Organisation Website: |
http://www.imperial.ac.uk |