With the continuing need for new air vehicle systems with aero-engines, there is a need for closer integration of the propulsion system and the airframe. With the timely development of new measurement methods, computational tools and optimisation systems it is envisaged that this design challenge can be addressed. The overall aim of the PhD project is to develop, validate and transfer to the sponsor an aerodynamic design and optimisation methodology for complex aero-engine intakes. The research will encompass both computational and experimental elements. The project is in collaboration with the UK Defence Science and Technology Laboratory and is fully funded for fees and bursary.
The integration of an aero-engine with the aircraft poses several aerodynamic challenges with respect to intake design. This applies to current podded type configurations as well as to more embedded installation configurations. Current research at Cranfield University is developing methods for the design, optimisation and analysis of a wide range of intake configurations. In addition, novel experimental methods have been applied to the evaluation of the unsteady distorted flow fields for complex intakes.
The aim of the research is to develop and validate a design and optimisation methodology for complex aero-engine intakes. The research will include the calculation and state of the art measurements of the complex, unsteady flow distortion which are at the heart of this intake design challenge. As part of the work, a range of optimisation methods will be investigated and a tool will be developed and applied to a specific intake configuration. The software will be configured to work with a range of CFD flow solvers. The project will contribute to the solution of a long-standing engineering challenge, whilst at the same time providing the investigator with an exceptional development opportunity through their engagement with DSTL. The research will encompass both computational and experimental aspects.
Part of the research will include a placement at DSTL for up to 3 months working with specialists to gain a broader appreciation of the range of applicability of the research.
Entry requirements
Applicants for the post must have a first-class or upper second-class degree in engineering or a related area. An aerospace background would be a distinct advantage as would experience of Python coding, computational aerodynamics, and experimental aerodynamics.
Although there is a nominal closing date of 30 April 2022, the post will be filled as soon as possible for a suitable candidate.
How to apply
For further information please contact:
Prof David MacManus
Email: [Email Address Removed]
If you are eligible to apply for this studentship, please complete the online application form.
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