| EPSRC Reference: |
GR/L95700/01 |
| Title: |
ADJOINT CFD ALGORITHMS FOR AERONAUTICAL DESIGN |
| Principal Investigator: |
Giles, Professor M |
| Other Investigators: |
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| Researcher Co-Investigators: |
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| Project Partners: |
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| Department: |
Computer Science |
| Organisation: |
University of Oxford |
| Scheme: |
Standard Research (Pre-FEC) |
| Starts: |
01 June 1998 |
Ends: |
31 May 2001 |
Value (£): |
104,245
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| EPSRC Research Topic Classifications: |
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| EPSRC Industrial Sector Classifications: |
| Aerospace, Defence and Marine |
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Summary on Grant Application Form |
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This proposal concerns the development and validation of adjoint CFD mathods for three design problems, determining the influence of design changes on steady-state performance, levels of forced response due to unsteady interactions, and the susceptibility to flutter. For the first of these, the aim is to improve upon the methods very recently developed in the US, The latter two are completely novel applications of adjoint equations for design. The benefit of the adjoint approach, in contrast to the iterative analysis approach to design, is very greatly reduced computational costs when there are large numbers of design variables, which will greatly speed up the design process.
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Key Findings |
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This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
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Potential use in non-academic contexts |
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This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
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Impacts |
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| Description |
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk |
| Summary |
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| Date Materialised |
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Sectors submitted by the Researcher |
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This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
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| Project URL: |
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| Further Information: |
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| Organisation Website: |
http://www.ox.ac.uk |