Aerodynamics of Static and Dynamic Stall – An Experimental Study
Aerodynamics and Flight Mechanics
Dr B Ganapathisubramani, Dr R De Kat
1 April 2019
Most aerofoils are operated at high angles of attack to maximise aerodynamic performance where they are prone to separation and stall, especially when they are operating under varied conditions.
Aero-engine installation aerodynamics PhD
Dr D MacManus
22 April 2019
The project is sponsored by the EU CleanSky Project and the work will be in collaboration with Rolls-Royce and the UK Aircraft Research Association.
Aircraft flutter suppression using plasma
Dr W Wang
Applications accepted all year round
Aircrafts can be lighter when composites are using. The structure would become more ‘flexible’, particularly for the wings. To prevent catastrophic structural failure from resonance coupled with aerodynamic loads, prevention and suppression of flutter are critical to design and operate air vehicles.
Investigation of Large Fold Angles of a Semi Aeroelastic Hinged Wing Tip
Prof J Cooper
31 March 2019
The Semi Aeroelastic Hinged wing tip concept has been developed by Airbus with the University of Bristol and is based on idea of allowing a wing-tip, that can be moved on the ground to fit airport gates, to be released for passive movement in-flight to enable gust loads alleviation & improved roll efficiency.
Development of CFD Methods for Future Digital Aircraft Design
Dr S Timme
31 August 2019
Do you want to be part of the team that is developing the next-generation computational fluid dynamics (CFD) software solution to be used by Airbus and partner organisations across Europe in the next decades?.