Output details
15 - General Engineering
University of Oxford
Influence of Film Cooling Hole Angles and Geometries on Aerodynamic Loss and Net Heat Flux Reduction
This research was undertaken under my direction at the Whittle Laboratory (Cambridge) when I worked at Rolls-Royce, Derby. It focuses on a careful study on the effect of film cooling hole shape on aerodynamic loss and film cooling effectiveness. The research improved design practice at Rolls-Royce and is an example of academic/industrial collaboration. The programme involved the development of heat transfer measurement capability at the Whittle Laboratory – a capability that has been put to good use in subsequent research. The collaboration between myself, Rolls-Royce and Cambridge strengthened our recent application for an EPSRC CDT in Aerodynamics.