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blade aerodynamics, gust interactions, and fluid-structure interactions. The research focuses on unfolding the origin and development of unsteady flow separation and vortex formation. The lab has built a
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studying across a number of UK Universities. The objective of the research is to understand the effects of structural warpage due to heating on the aerodynamic performance of supersonic intakes and then
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), different sets of samples will be prepared to conduct microscopic and rheological characterisations. Afterwards, further samples will be prepared that will undergo various mechanical tests (e.g., viscoelastic
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behaviour across different regimes. These simulations will provide critical insights into the effects of various porous structures on aerodynamic performance. Additionally, the project involves the creation
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research projects across areas such as: Zero Emission Technologies. Ultra Efficient Aircraft, Propulsion, Aerodynamics, Structures and Systems. Aerospace Materials, Manufacturing, and Life Cycle Analysis
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these goals in different research frameworks and collaborative re-search with industry partners. Requirements Profile The following requirements apply for the position at the offer: • Excellent grade degree
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investigation of the aerodynamic performance of advanced future compressor stages, support-ed by numerical modelling and simulations of performance-enhancing design features. In this research project you will be