European and Industrial projects
- H2020 – SMS - Smart Morphing and Sensing for aeronautical configurations,
IMFT Toulouse
- Cooperative Research for Next Generation High Efficiency LP Turbine,
Coordinator AVIO Aero Poland
- 7th FP Transition Location Effect on Shock Wave Boundary Layer Interaction (TFAST),
Coordinator IMP PAN
- 7th FP Full Aerothermal Combustor-Turbine Interactions Research (FACTOR),
Coordinator Snecma Moteurs
- 7th FP Engine Representative Internal Cooling Knowledge and Applications (ERICKA),
Coordinator Rolls-Royce plc.
- Impinging jet cooling - LuFo-4 Robusturb cooperation with Rolls-Royce Deutschland
- Aerodynamic and aero-acoustic analysis of W-3A Falcon helicopter main rotor,
Institute of Aviation, PZL-Świdnik
- 6th FP Towards Lean Combustion (TLC),
Coordinator Snecma
- 6th FP Unsteady effects of shock wave induced separation (UFAST),
Coordinator IMP PAN
- 6th FP Flight Reynolds Testing Number (FLIRET),
Coordinator Airbus
- 6th FP Aerothermal Investigation of Turbine Endwalls and Blades – 2 (AITEB-2)
- 5th FP Aerothermal Investigation of Turbine Endwalls and Blades (AITEB),
Coordinator Rolls-Royce Deutschland
- 5th FP Innovative Aerodynamic High-Lift Concepts (HELIX) (subcontractor)
- EUROSHOCK I and II (1994-1999,DLR) - shock wave boundary layer interaction and its passive and active control.
