-
. The overall aim of this PhD project is to analyse droplet impact mechanics along with the freezing thermodynamics under high airspeeds to gather important insights into ice adhesion behaviour. The experiments
-
, including SuperMagdrive, operates using metallic propellant, offering density, integration, and safety advantages compared to conventional launcher propellants such as hydrazine. However, metal propellants
-
across rockets/launch vehicles, satellites, and space stations, primarily due to their potential for significant weight reduction while maintaining superior mechanical performance. One of the key
-
this project, the student will gain highly sought-after expertise in experimental fluid mechanics which is a key identified area of growth to enable development of next generation power and propulsion systems
-
EligibilityUK, EU, Rest of world Reference numberSATM568 Entry requirements Applicants should have either a UK or UK-equivalent first or second-class honours degree in mechanical engineering, aerospace
-
mechanism. The integrating should enable to guarantee certain properties of the learned functions, while keep leveraging the strength of the data-driven modelling. Most of, if not all, the traditional