Jason Krawciw MEng
Combustion system aerodynamics, Heat transfer and cooling, Experimental fluid mechanics, Computational fluid dynamics
Member of the Rolls-Royce UTC in Combustion System Aerothermal Processes since 2012.
- Combustor effusion cooling systems
- Experimental and computational study of gas turbine aerodynamics and combustion system aerothermal processes.
- PhD, ‘Optimisation techniques for combustor wall cooling’, Loughborough University, To be completed mid 2016
- MEng(hons) Aeronautical Engineering, Loughborough University, 2012
- Research Student, Research Associate, Rolls-Royce University Technology Centre in Combustion Aerodynamics, Loughborough University, 2012-present.
- Engineering Intern, Rolls-Royce Plc 2010-2011
Experimental and computational study of combustor liner cooling flows in modern gas turbines. Focus on effusion cooling designs including novel cooling hole geometries.
Selected research projects:
SILOET 2 – Novel effusion cooling concepts for DLD combustors – 2013-2015.
Member if the Rolls-Royce UTC in Combustion System Aerothermal Processes
Publications and Awards
2015 - ‘Measurement and prediction of adiabatic film effectiveness of combustor representative effusion arrays’ ASME GT2015-43210