Although there is a nominal closing date of 10th September 2021, the post will be filled as soon as possible for a suitable candidate.
Introduction
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.
Background
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.
The student will be based within the School of Aerospace, Transport and Manufacturing. Cranfield operates a substantial Doctoral Researchers Core Development programme (DRCD) for its research students. This programme is based on the Researcher Development Framework which is the national professional development framework for supporting researchers not just during the PhD but also throughout their career. This system provides a generic structured training programme which is constructed to support the researcher as the PhD progresses with specific courses aimed at the different phases of a PhD. For example, the programme includes aspects such as research methods, technical report writing, presenting research, data management, leadership skills, professional development planning, intellectual property, publishing, etc. Cranfield is a wholly post-graduate university and there are a wide range of MSc and Professional Development Short Courses throughout the year. These mainly focus on technical topics and a specific training programme will be agreed with the PhD student.
About the sponsor - This studentship is sponsored by EPSRC and UK DSTL ICASE. A stipend of £15,609 per annum (tax free) plus UK tuition fees applies.
Funding - To be eligible for this funding, applicants must be a UK national. Applicants must also clear administrative checks from the sponsor.
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.
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