Integrated Aircraft Dynamic Loads Analysis for Multidisciplinary Design Optimization of Flexible Transport Aircraft. (Filled)
- Development of Aircraft Dynamic Simulation Tool Based on Aeroelastic Integral Model of Flexible Aircraft. (Open)
Theoretical and Experimental Characterisation and Performance Optimisation of Fibre Metal Laminates Subject to Quasi-Static and Dynamic Loading.(Filled)
- Interface Mechanics of Fibre Metal Laminates with Mechanical Interlock Bonding System (Damage Tolerance and Crack Bridging). (Open)
N.B. there may be opportunities for the students to spend time at the facilities of our industrial partners.