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Assessment of Future Aero Engine Designs with Intercooled and Intercooled Recuperated Cores
Cranfield University, UK.ORCID iD: 0000-0002-8466-356X
Chalmers University of Technology, Sweden.
Cranfield University, UK.
Cranfield University, UK.
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2010 (English)Conference paper, Published paper (Refereed)
Abstract [en]

Reduction in CO 2 emissions is strongly linked with the improvement of engine specific fuel consumption, as well as the reduction in engine nacelle drag and weight. Conventional turbofan designs, however, that reduce CO 2 emissions—such as increased overall pressure ratio designs—can increase the production of NO x emissions. In the present work, funded by the European Framework 6 collaborative project NEW Aero engine Core concepts (NEWAC), an aero-engine multidisciplinary design tool, Techno-economic, Environmental, and Risk Assessment for 2020 (TERA2020), has been utilized to study the potential benefits from introducing heat-exchanged cores in future turbofan engine designs. The tool comprises of various modules covering a wide range of disciplines: engine performance, engine aerodynamic and mechanical design, aircraft design and performance, emissions prediction and …

Place, publisher, year, edition, pages
2010.
National Category
Aerospace Engineering
Research subject
Energy- and Environmental Engineering
Identifiers
URN: urn:nbn:se:mdh:diva-43163DOI: 10.1115/GT2010-23621OAI: oai:DiVA.org:mdh-43163DiVA, id: diva2:1305961
Conference
ASME TURBO EXPO 2010 Proceedings, paper no. GT2010-23621
Available from: 2019-04-21 Created: 2019-04-21 Last updated: 2019-06-03Bibliographically approved

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Kyprianidis, Konstantinos

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