Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/29309
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dc.contributor.authorSalah, SI-
dc.contributor.authorWhite, MT-
dc.contributor.authorSayma, AI-
dc.date.accessioned2024-07-07T11:25:02Z-
dc.date.available2024-07-07T11:25:02Z-
dc.date.issued2022-05-14-
dc.identifierORCiD: Salma I. Salah https://orcid.org/0000-0001-7541-1320-
dc.identifierORCiD: Abdulnaser I. Sayma https://orcid.org/0000-0003-2315-0004-
dc.identifier100156-
dc.identifier.citationSalah, S.I., White, M.T. and Sayma, A.I. (2022) 'A comparison of axial turbine loss models for air, sCO<inf>2</inf> and ORC turbines across a range of scales', International Journal of Thermofluids, 15, 100156, pp. 1 - 22. doi: 10.1016/j.ijft.2022.100156.en_US
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/29309-
dc.description.abstractLoss models are used to evaluate the aerodynamic performance of axial turbines at the preliminary design stage. The commonly used loss models were derived for air and steam turbines and have not been sufficiently investigated for turbines working with non-conventional working fluids, relevant to new power systems, such as organic fluids and supercritical CO2 (sCO2). Thus, the aim of this study is to explore the deviation between the performance predictions of different loss models, namely Dunham and Came, Kacker and Okapuu, Craig and Cox and Aungier, for non-conventional working fluids where turbines may differ in design and operation than conventional air or steam turbines. Additionally, this paper aims to investigate the effect of the turbine scale on the trends in the performance predictions of these models. Three different case-studies are defined for air, organic Rankine cycle (ORC) and sCO2 turbines and each one is evaluated at two different scales. It is found that the selected loss models resulted in varying loss predictions; particularly for predicting the losses due to the clearance gap for all small scale designs. Furthermore, large variations were found in predicting the effect of the flow regime on the turbine performance for all models.en_US
dc.description.sponsorshipEuropean Union’s Horizon 2020 research and innovation programme under grant agreement No. 814985.en_US
dc.format.extent1 - 22-
dc.format.mediumElectronic-
dc.languageEnglish-
dc.language.isoen_USen_US
dc.publisherElsevieren_US
dc.rightsCrown Copyright / The Authors © 2022 Published by Elsevier Ltd. This is an open access article under the CC BY license (https://creativecommons.org/licenses/by/4.0/).-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.subjectperformance analysisen_US
dc.subjectnon-conventional working fluidsen_US
dc.subjectloss modelsen_US
dc.subjectair turbinessen_US
dc.subjectCO2 turbinesen_US
dc.subjectORC turbinesen_US
dc.titleA comparison of axial turbine loss models for air, sCO<inf>2</inf> and ORC turbines across a range of scalesen_US
dc.typeArticleen_US
dc.date.dateAccepted2022-04-30-
dc.identifier.doihttps://doi.org/10.1016/j.ijft.2022.100156-
dc.relation.isPartOfInternational Journal of Thermofluids-
pubs.publication-statusPublished-
pubs.volume15-
dc.identifier.eissn2666-2027-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dc.rights.holderCrown Copyright / The Authors-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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