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Centre for Propulsion and Thermal Power Engineering and specifically the Rolls-Royce UTC in Aero Systems Design, Integration and Performance . This role will contribute to the development of various
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. This exciting new role is co-developed with the Defence Science and Technology Laboratory (DSTL) and dedicated to the identified future research areas of novel human-swarm teaming in complex scenarios. About the
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Aerospace – Centre for Propulsion & Thermal Power Engineering Research Fellow in Fluid Dynamics for Aero System Design Fixed Term Contract until 30 September 2026 Full time starting salary is normally in
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for commercial aircrafts. The vision is to develop a new design and manufacturing technology for landing gear using advanced additive manufacture, novel materials and new design methods. This will contribute to a
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addition to, and outside of, normal working hours. About You You must have BTEC/HNC or A levels in science/engineering-based subjects or equivalent qualifications. To succeed in this role, you will have demonstrable
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-physical Systems at Cranfield. This exciting new role is co-developed with the Defence Science and Technology Laboratory (DSTL) and dedicated to the identified future research areas of novel human-swarm
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We welcome applications for this key post from those with the relevant research and teaching experience in the area of surface engineering coating manufacturing methods, with the ability to set up and
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to develop a new design and manufacturing technology for landing gear using advanced additive manufacture, novel materials and new design methods. This will contribute to a new landing gear design
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of preparing engineers to develop new products for the nascent British aerospace industry. We've been teaching aeronautics-related topics ever since, either through our world-class post graduate MSc courses
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applications from engineers - scientists with expertise in computer engineering and/or programming and/or algorithm deployment within the aviation sector covering intelligent sensing and acquisition and