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are computationally prohibitive, which limits their applicability to a restricted set of parameters and configurations. In this project, we aim to develop novel analytical and reduced-order numerical methods
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phenomena in other fluid–structure systems, but a systematic application to ABS geometries and conditions has not yet been undertaken. This PhD project aims to address this gap by: 1. Developing a numerical
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to mix. In specialized heat exchangers developed for air-breathing rocket engines (Varvill, 2010), the strong reduction in tube diameter may lead to excessive tube failures caused by flow-induced
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develop a research and training programme that bridges the current divide between space engineering and climate science to close the gaps that exist in the Life-Cycle Analysis of space launch systems. Thus