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The Effect of Engine Dimensions on Supersonic Aircraft Performance

Alvaro Abdalla ; Henrique Gazetta ; Tomas Grönstedt (Institutionen för tillämpad mekanik, Strömningslära) ; Petter Krus
4:th CEAS Air & Space Conference (2013)
[Konferensbidrag, refereegranskat]

In aircraft design a critical part of the design is the engine selection. This is typically making a selection from exiting engines. Looking at a next generation future fighters, however, where the time of deployment may be 20-30 years in the future this is not a valid approach as there will be an evolution in the engine designs. E.g. a new European fighter aircraft will most likely be a collaborative project also involving the development of an engine for that aircraft. In this study conceptual engine-airframe co-design is demonstrated, using models of comparable fidelity for both the engine design and the aircraft design. This co-design leads to a deeper understanding of the tradeoffs from both sides, and means that also more radical designs and innovations can be evaluated in a fair way.

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Denna post skapades 2013-12-19.
CPL Pubid: 189924


Institutioner (Chalmers)

Institutionen för tillämpad mekanik, Strömningslära (2005-2017)


Innovation och entreprenörskap (nyttiggörande)
Rymd- och flygteknik

Chalmers infrastruktur