Sort by
Refine Your Search
-
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
-
of £37,337 per annum We welcome applications for this key research post in partnership with Rolls-Royce from those with relevant knowledge and experience in fluid dynamic design and analysis of systems used in
-
the range of £28,203 to £30,440 per annum Location: Cranfield, Bedfordshire We welcome applications from prospective Research Assistants in Human-centred AI, with experience in designing, developing, and
-
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
-
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
-
experience in designing, developing, and validating novel human-swarm collaboration framework with effective AI and augmented reality technologies. Applicant will work in the Centre for Autonomous and Cyber
-
of Net Zero UK by 2050. We offer world-class and niche post-graduate level research, education, training and consultancy. We are unique in our multi-disciplinary approach by bringing together design
-
of Net Zero UK by 2050. We offer world-class and niche post-graduate level research, education, training and consultancy. We are unique in our multi-disciplinary approach by bringing together design
-
Centre, Cranfield, Bedfordshire We are looking for an experienced individual to help design and deliver a decision support software for assessing pressures and impacts on river ecology, that will be used
-
contribute to sustainable aviation advances. About the Role You will be working closely with world leading researchers and industrial engineers on the aerodynamic design and analysis of aero-engine intake