104 structural-engineering "https:" "https:" "https:" "https:" "https:" "https:" "Multiple" positions at University of Bristol
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suitable area of ML/AI applied to engineering problems relevant to the School; for example aerodynamics, fluids, aeroacoustics, composite structures, structural mechanics, flight dynamics, control. A proven
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supports people to achieve their potential, please see our staff blog: https://engineering.blogs.bristol.ac.uk/category/engineering-includes-me/ Contract type: Open ended Work pattern: Full time Grade: H
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supports people to achieve their potential, please see our staff blog: https://engineering.blogs.bristol.ac.uk/category/engineering-includes-me/ Contract type: Open ended Work pattern: Full time Grade: J
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supports people to achieve their potential, please see our staff blog: https://engineering.blogs.bristol.ac.uk/category/engineering-includes-me/ Contract type: Open ended Work pattern: Full time Grade: J / K
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comfortable liaising across multiple teams and differing stakeholders, including industry, academics and people within the maker/hacker community. They will work closely with several IT teams to develop and
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supports people to achieve their potential, please see our staff blog: https://engineering.blogs.bristol.ac.uk/category/engineering-includes-me/ Contract type: Open ended Work pattern: Full time Grade: J/K/L
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that can deliver complex, high-integrity and scalable reactor components. This PhD project will focus on the engineering of additive manufacturing (AM) to support the design and fabrication of resilient
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and conferences in the field of composite materials, structural mechanics and engineering science. In addition to the research, the role holder may, where practical, contribute to teaching, through co
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development and eager to contribute to a pioneering academic venture. You can apply for the role at the below link - https://emeritus.darwinbox.in/ms/candidate/careers/a691c12f9b618a To complete your
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processes. You will be based at Rolls-Royce in Derby, and work on the development and validation of numerical methods for predicting the structural integrity of composite components for aircraft engines in