Development of a Design Synthesis Methodology Appropriate to the Conceptual Design of 6th Generation Combat Aircraft PhD

This PhD topic relates tool development appropriate to the conceptual design of 6th generation combat aircraft. The research will explore relevant feature modelling and progress to explore the design space of this class of vehicle.

An existing design methodology is being developed to assist the knowledgeable aircraft designer in developing conceptual designs of aircraft. To date this has primarily focussed on a wide range of civil applications, but recent research has looked to extending the approach to military aircraft. The intent of this study is to further develop the method to military applications. Fee bursary available to UK student

This topic relates tool development appropriate to the conceptual design of 6th generation combat aircraft. The research will explore relevant feature modelling and progress to explore the design space of this class of vehicle.

An existing design methodology is being developed to assist the knowledgeable aircraft designer in developing conceptual designs of aircraft. To date this has primarily focussed on a wide range of civil applications, but recent research has looked to extending the approach to military aircraft. The intent of this study is to further develop the method to military applications.

The existing tool makes use of various interacting modules, operating at differing levels of fidelity, each responsible for a specific design aspect (e.g., Aerodynamics, Mass and Balance, Performance etc.). By manipulating input and other control parameters, one can obtain a broad range of aircraft configurations and results. This method should allow the development of a conceptual design tool tailored for designing future combat aircraft, while also allowing extensive parametrisation of design features and flexibility, thus providing an excellent tool for cost-effective trade or validation studies. Its modular nature may also allow additional features, to be studied and their effect on the overall design and performance to be established, effectively and quickly.

This project will focus on the 6th generation combat aircraft and will likely consider features such as directed energy weapon systems, low observable technologies in addition to considering both crewed and de-crewed concepts.

There is considerable interest in this class of vehicle and so (subject to Export License) good publications should be forthcoming.

• Application deadline08 May 2024
• Award type(s)PhD
• Start date30 Sep 2024
• Duration of award3 years
• EligibilityUK
• Reference numberSATM457

Applicants should have a first or second class UK honours degree or equivalent in Aeronautical Engineering or aerospace or a related discipline. This project would suit those with a strong interest in aviation. Experience of computer programming (preferably in Java) would be an advantage. A logical, creative mind would be appropriate.

Applicants should be UK Nationals.

Sponsored by Cranfield University.

Bursary covers tuition fees for 3 years.

Research students at Cranfield benefit from being part of a dynamic, focused and professional study environment and all become valued members of the Cranfield Doctoral Network.  This network brings together both research students and staff, providing a platform for our researchers to share ideas and collaborate in a multi-disciplinary environment. It aims to encourage an effective and vibrant research culture, founded upon the diversity of activities and knowledge. A tailored programme of seminars and events, alongside our Doctoral Researchers Core Development programme (transferable skills training), provide those studying a research degree with a wealth of social and networking opportunities.

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

For further information please contact

Professor Howard Smith
E: [email protected]