EPSRC logo

Details of Grant 

EPSRC Reference: GR/M22260/01
Title: COUPLED AERO-STRUCTURAL CALCULATIONS FOR WINGS IN UNSTEADY TRANSONIC FLOWS
Principal Investigator: Allen, Professor CB
Other Investigators:
Lieven, Professor N
Researcher Co-Investigators:
Project Partners:
Airbus Group Limited BAE Systems Ministry of Defence (MOD)
Department: Aerospace Engineering
Organisation: University of Bristol
Scheme: Standard Research (Pre-FEC)
Starts: 01 April 1999 Ends: 30 September 2002 Value (£): 169,868
EPSRC Research Topic Classifications:
Aerodynamics
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine
Related Grants:
Panel History:  
Summary on Grant Application Form
A nonlinear method for computing the combined unsteady aero-structural response of a wing i transonic flow will be developed, with application to flutter boundary prediction. The method will combine an existing efficient solver for unsteady flows with moving meshes and modal/FE structural model. 'Strong' coupling of the aero and structural methods will be achieved by use of the dual-time approach. Fully nonlinear, 'datum' solutions will be obtained. A preliminary investigation of the effects of linearised and semi-linear methods for the flow prediction will be carried out. The effects of some types of structural nonlinearities on the coupled response will also be examined.
Key Findings
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Potential use in non-academic contexts
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Impacts
Description This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Summary
Date Materialised
Sectors submitted by the Researcher
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
Project URL:  
Further Information:  
Organisation Website: http://www.bris.ac.uk