| EP/N024354/1 | Analysis and Design for Accelerated Production and Tailoring of composites (ADAPT) | (P) |
| EP/K031368/1 | Multiscale Modelling of Aerospace Composites: Increasing Quality, Reducing Empiricism and Challenging Conservatism | (P) |
| EP/H025898/1 | Aerostructural Efficiency of Damage Tolerant Composites via Optimised Fibre Placement | (P) |
| EP/F026099/1 | Equipment for Multiple Projects: Testing and Visualization for Aerospace Research | (P) |
| GR/R54828/01 | THE EFFECT OF DELEMAINATION DAMAGE ON THE COMPRESSIVE STRENGHTH AND FATIGUE LIFE OF AEROSPACE COMPOSITES | (C) |
| GR/M26220/01 | INITIAL AND ADVANCED POST-BUCKLING OF OPTIMIZED STIFFENED PANELS | (C) |
| GR/M26237/01 | INITIAL AND ADVANCED POST-BUCKLING OF OPTIMIZED STIFFENED PANELS | (C) |
| GR/K85667/01 | CONCEPTUAL DESIGN OF COMPOSITE WING STRUCTURES WITH AEROELASTIC,STRENGTH & MANUFACTURING CONSTRAINTS | (C) |
| GR/K87623/01 | CONCEPTUAL DESIGN OF COMPOSITE WING STRUCTURES WITH AEROELASTIC STRENGTH AND MANUFACTURING CONSTRAINTS | (P) |
| GR/H78467/01 | AEROELASTIC OPTIMISATION OF COMPOSITE WINGS | (P) |
| GR/H17572/01 | PRACTICAL ENHANCEMENT OF VICONOPT AN EFFICIENT BUCKLING DESIGN PROGRAM FOR AEROSPACE STRUCTURES | (P) |