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Contribution to knowledge I. Contribution to the development of a multi-disciplinary aero engine concep- tual design tool, within a collaborative environment. The tool is based on an explicit algorithm and is targeted towards identifying an appropri- ate design space where more complex and time-consuming tools could be utilised. The author’s efforts focused on the development of (i) a new engine performance code, (ii) a numerical methods library, (iii) a new emissions prediction and environmental impact code, (iv) and the enhancement of existing codes for engine lifing, direct operating costs and aircraft design and performance. II. Assessment of future environmentally friendly jet engine systems, using the developed tool, including: • Assessment of the impact of thermo-fluid modelling uncertainties on performance calculations and emissions predictions at aircraft system level, and identification of accuracy limitations in assessing novel con- cepts as imposed by current practice in thermo-fluid modelling. • Quantification of potential benefits from low pressure spool technolo- gies for three turbofan architectures and the impact of failing to deliver specific component technologies, for long and short range applications. • Quantification of potential benefits from the introduction of heat- exchanged cores in turbofan engines and identification of fuel optimal designs for year 2020 entry into service, for long range applications. It is likely that detailed studies and such tools exist internally in companies. Nevertheless, it is worth having such a tool and future aero engine assessments available for the broader research community. Whilst the detailed publications and the work carried out by the author, in a collaborative effort with other project partners, is presented in the main body of this thesis, it is important to note that this work is supported by 20 conference and journal papers. iiiPDF Image | Multi-disciplinary conceptual design of future jet engine systems
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