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Details of Grant 

EPSRC Reference: GR/L95700/01
Title: ADJOINT CFD ALGORITHMS FOR AERONAUTICAL DESIGN
Principal Investigator: Giles, Professor M
Other Investigators:
Researcher Co-Investigators:
Project Partners:
BAE Systems Rolls-Royce Plc
Department: Computer Science
Organisation: University of Oxford
Scheme: Standard Research (Pre-FEC)
Starts: 01 June 1998 Ends: 31 May 2001 Value (£): 104,245
EPSRC Research Topic Classifications:
Aerodynamics
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine
Related Grants:
Panel History:  
Summary on Grant Application Form
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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Organisation Website: http://www.ox.ac.uk