Aeronautical Design Group
Faster, cleaner, safer flight
The aim of this group is to research the role of computational models in the delivery of highly interactive technical systems:
- by developing high performance design optimisation approaches;
- by studying the use of robust computational design in aerospace systems;
- by investigating the aerodynamic design of shock control bumps for swept transonic flows.
The group is currently collaborating with compressor and turbine aerodynamics specialists at Rolls Royce, UK.