14 information-security "https:" "https:" "https:" "https:" "https:" "Dr" "Robert Gordon University" PhD positions at Imperial College London
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London in this area, go to: https://www.imperial.ac.uk/mechanical-engineering/research/ For information on how to apply, go to: http://www.imperial.ac.uk/mechanical-engineering/study/phd/how-to-apply
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, go to: https://www.imperial.ac.uk/mechanical-engineering/research/ For information on how to apply, go to: http://www.imperial.ac.uk/mechanical-engineering/study/phd/how-to-apply/ For further details
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start date would be preferred if possible. For informal enquiries about the project, please contact Dr Adrià Junyent‑Ferré (adria.junyent-ferre@imperial.ac.uk ). To apply, please complete the Expression
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: Aeronautics Research (PhD) Research Topic:Please use reference number AE0086 Research Supervisor: Dr Anh Khoa Doan Research Group:Aero For further information: For questions about the project, please contact
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, please contact Dr Jun Jiang at jun.jiang@imperial.ac.uk . Further information on research in mechanical engineering at Imperial College London can be found at: https://www.imperial.ac.uk/mechanical
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) and the industrial supervisor is Dr Stefanos Giannis (NPL) Duration: 4 years. Funding: Full coverage of tuition fees and an annual tax-free stipend of £22,780 for Home students. Find out more about fee
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of rain drops by purely thermodynamic means is not possible in such a short time scale highlighting the importance of turbulence within clouds to these processes. Cloud turbulence causes collision between
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retention across the Dengue and Zika Immunology and Genomics Multi-Country Network (DeZi Network). DeZi is a new Wellcome Trust-funded programme, delivered with the World Health Organization, national
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Supervisors: Professor Victoria Cornelius, Dr Hadith Rastad, Dr Tim Rawson About the role Sequential Multiple Assignment Randomised Trials (SMARTs) are increasingly used to evaluate multistage
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), accounting for dynamic aeroelastic stability at the early design stage has become essential. However, considering flutter constraints in high-fidelity aerostructural optimisation routines is challenging