Part 2: Design Optimisation Strategies for a Fuel Spray Nozzle

Andreou, T., White, C. , Kontis, K. , Shahpar, S. and Brown, N. (2021) Part 2: Design Optimisation Strategies for a Fuel Spray Nozzle. In: ASME 2020 Turbo Expo Conference (TE20), 21-25 Sept 2020, ISBN 9780791884089 (doi: 10.1115/GT2020-15431)

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Reducing emissions and improving fuel economy has become a key target for advanced aircraft engine platforms. The competitive aviation market requires a drastic reduction in current aircraft emission levels, which leads to the requirement of optimising the entire combustion process. Lean burn pre-mixed systems are an efficient way of reducing NOx emissions. Starting from a datum blade generated in a companion paper, shape optimisation strategies applied to a fuel spray nozzle have been explored. Making use of three different design space parametrisation methods and several optimisation algorithms, an optimised passage has been generated. The optimised design achieves a considerable pressure loss reduction in comparison to the baseline design.

Item Type:Conference Proceedings
Additional Information:We would like to thank Rolls-Royce Plc and the University of Glasgow for the provision of funding, high-performance computational resources, and software, without which this research could not have been completed.
Glasgow Author(s) Enlighten ID:Kontis, Professor Konstantinos and Andreou, Mr Thomas and White, Dr Craig
Authors: Andreou, T., White, C., Kontis, K., Shahpar, S., and Brown, N.
College/School:College of Science and Engineering > School of Engineering
College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity
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