Adopting exergy analysis for use in aerospace

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dc.contributor.author Hayes, David
dc.contributor.author Lone, Mudassir
dc.contributor.author Whidborne, James F.
dc.contributor.author Camberos, José
dc.contributor.author Coetzee, Etienne
dc.date.accessioned 2017-10-23T08:11:31Z
dc.date.available 2017-10-23T08:11:31Z
dc.date.issued 2017-08-05
dc.identifier.citation David Hayes, Mudassir Lone, James F. Whidborne, José Camberos, Etienne Coetzee, Adopting exergy analysis for use in aerospace, Progress in Aerospace Sciences, Volume 93, 2017, Pages 73-94 en_UK
dc.identifier.issn 0376-0421
dc.identifier.uri https://doi.org/10.1016/j.paerosci.2017.07.004
dc.identifier.uri https://dspace.lib.cranfield.ac.uk/handle/1826/12664
dc.description.abstract Thermodynamic analysis methods, based on an exergy metric, have been developed to improve system efficiency of traditional heat driven systems such as ground based power plants and aircraft propulsion systems. However, in more recent years interest in the topic has broadened to include applying these second law methods to the field of aerodynamics and complete aerospace vehicles. Work to date is based on highly simplified structures, but such a method could be shown to have benefit to the highly conservative and risk averse commercial aerospace sector. This review justifies how thermodynamic exergy analysis has the potential to facilitate a breakthrough in the optimization of aerospace vehicles based on a system of energy systems, through studying the exergy-based multidisciplinary design of future flight vehicles. en_UK
dc.language.iso en en_UK
dc.publisher Elsevier en_UK
dc.rights Attribution-NonCommercial-NoDerivatives 4.0 International
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject Exergy en_UK
dc.subject Thermodynamics en_UK
dc.subject Multi disciplinary optimisation en_UK
dc.title Adopting exergy analysis for use in aerospace en_UK
dc.type Article en_UK


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