Rolls Royce UTCin Combustion System Aerothermal Processes


Jason Krawciw MEng

Photo of  Jason Krawciw

Research Associate

Research Group:
Applied Aerodynamics

Research Interests:
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

Past Positions:

  • 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.

External Activities

Member if the Rolls-Royce UTC in Combustion System Aerothermal Processes

Publications and Awards

View Publications for Jason Krawciw

2015 - ‘Measurement and prediction of adiabatic film effectiveness of combustor representative effusion arrays’ ASME GT2015-43210