13 information-security "https:" "https:" "https:" "https:" "Adolescent Health Study (AHS)" PhD positions at Imperial College London in United Kingdom
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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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https://www.imperial.ac.uk/mechanical-engineering/study/phd/how-to-apply/ and select “PhD in Mechanical Engineering – Materials and Manufacturing” before uploading your documents. For informal enquiries
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will develop and evaluate fault detection and fault location algorithms for these systems. The project is funded by GE Vernova under a wider collaboration with Imperial College London. You will be co
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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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Start Date: 01/10/2026 Application deadline: 26/03/2026 Applications are invited for a fully-funded Ph.D. studentship in the Department of Aeronautics in structural power composites. This PhD is
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Start Date: As soon as possible Application deadline: 1st April 2026 Introduction: Climate change and the race to decarbonize our society is making extreme events in fluids more prevalent. These
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part of the NURISH (NURturing transformative capacities, Innovation in NBS and Harmonious resilience in rural areas) project. It is funded by the Horizon Europe Grant for Culture, creativity and
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comparisons. Second, reporting of initial and subsequent randomisation procedures is often incomplete. Third, primary aims and estimands are frequently unclear. Finally, embedded‑regime and tailored‑regime
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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