Aero-Engine Experimental Aerodynamics PhD

This is a full funded PhD (fees and bursary) in propulsion system aerodynamics in collaboration with Rolls-Royce and EPSRC. Fundamental understanding of aerodynamic flows is at the heart of aero-engine design and a key research area  is the ability to measure complex flow fields. Within that context, the overall aim of this PhD is to further develop non-intrusive laser-based flow measurement systems with new event-based cameras for stereo PIV measurements. This will be used to characterise the dynamic flow distortion within confined regions such as convoluted aero-engine intakes. This is expected to yield significant benefits in advanced aerodynamic measurements where there is a keen interest in obtaining measurements close to surfaces.

For future aircraft concepts there is an expectation that new architectures feature closer integration of the propulsion system with the airframe. A key challenge for such configurations will be the more complex aerodynamic characteristics associated with the propulsion system integration. Within that context there is an on-going interest is developing new flow measurement capabilities for new aero-engine configurations. Previous work within the group at Cranfield has demonstrated the use of stereo PIV methods for a range of aero-engine related topics such as intake ground vortex, distortion ingestion as well as the characterisation of unsteady flows for complex intake configurations. These have demonstrated the considerable benefits of PIV to provide rich flow field measurements which are unobtainable using conventional methods.  

For further information please contact:

Name: Professor David MacManus

Email: [email protected]

If you are eligible to apply for this studentship, please complete the online application form.