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aerodynamic characteristics associated with the propulsion system integration. This can apply to the aero-engine intake, exhaust, nacelle and main propulsion system. The overall aim of the funded PhD project is
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cities of Oxford and Cambridge. Our central location provides easy access from the M1, excellent main line rail service as well as proximity to key international airports. Set in rolling countryside
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Recently, aviation organizations have set severe targets to reduce emissions in the next generation of air travel systems. The main objective of this project is to contribute to these targets
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the efficiency improvement of the gas turbine architecture, combined with the use of Hydrogen or 100% SAF net zero carbon fuel as the main route to achieve its ambition of 30% greenhouse gases reduction by 2035
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the efficiency improvement of the gas turbine architecture, combined with the use of Hydrogen or 100% SAF net zero carbon fuel as the main route to achieve its ambition of 30% greenhouse gases reduction by 2035
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the efficiency improvement of the gas turbine architecture, combined with the use of Hydrogen or 100% SAF net zero carbon fuel as the main route to achieve its ambition of 30% greenhouse gases reduction by 2035
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digestates and the residual biogas potential (RBP) emitted from secondary open digesters, during dewatering or from cake pads remain unclear. This project recognises sludge treatment centres as the main source
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to enlist the main elastic and thermal properties. Later, the experiments will be performed and results will be analysed to empirically relate the elastic and thermal behaviour of the selected material
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this work focuses on, these aerodynamic interactions are due to the main rotor wake impinging on the tail rotor for certain operating conditions that depend on vehicle design characteristics
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performance degradations and unwarranted system failures can occur. There is certain physical information known a priori in such aerospace platform operations. The main research hypothesis to be tested in