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dc.contributor.authorLettieri, Claudio
dc.contributor.authorBryanston-Cross, Peter
dc.contributor.authorPaxson, Derek Edwin
dc.contributor.authorSpakovszky, Zoltan S
dc.date.accessioned2018-04-13T14:04:32Z
dc.date.available2018-04-13T14:04:32Z
dc.date.issued2017-11
dc.date.submitted2017-08
dc.identifier.issn0742-4795
dc.identifier.issn1528-8919
dc.identifier.urihttp://hdl.handle.net/1721.1/114689
dc.description.abstractCarbon capture and storage could significantly reduce carbon dioxide (CO₂) emissions. One of the major limitations of this technology is the energy penalty for the compression of CO₂ to supercritical conditions. To reduce the power requirements, supercritical carbon dioxide compressors must operate near saturation where phase change effects are important. Nonequilibrium condensation can occur at the leading edge of the compressor, causing performance and stability issues. The characterization of the fluid at these conditions is vital to enable advanced compressor designs at enhanced efficiency levels but the analysis is challenging due to the lack of data on metastable fluid properties. In this paper, we assess the behavior and nucleation characteristics of high-pressure subcooled CO₂ during the expansion in a de Laval nozzle. The assessment is conducted with numerical calculations and corroborated by experimental measurements. The Wilson line is determined via optical measurements in the range of 41-82 bar. The state of the metastable fluid is characterized through pressure and density measurements, with the latter obtained in a first-of-its-kind laser interferometry setup. The inlet conditions of the nozzle are moved close to the critical point to allow for reduced margins to condensation. The analysis suggests that direct extrapolation using the Span and Wagner equation of state (S-W EOS) model yields results within 2% of the experimental data. The results are applied to define inlet conditions for a supercritical carbon dioxide compressor. Full-scale compressor experiments demonstrate that the reduced inlet temperature can decrease the shaft power input by 16%.en_US
dc.publisherAmerican Society of Mechanical Engineers (ASME)en_US
dc.relation.isversionofhttp://dx.doi.org/10.1115/1.4038082en_US
dc.rightsArticle is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use.en_US
dc.sourceASMEen_US
dc.titleCharacterization of Nonequilibrium Condensation of Supercritical Carbon Dioxide in a de Laval Nozzleen_US
dc.typeArticleen_US
dc.identifier.citationLettieri, Claudio et al. “Characterization of Nonequilibrium Condensation of Supercritical Carbon Dioxide in a de Laval Nozzle.” Journal of Engineering for Gas Turbines and Power 140, 4 (November 2017): 041701 © 2018 ASMEen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.mitauthorPaxson, Derek Edwin
dc.contributor.mitauthorSpakovszky, Zoltan S
dc.relation.journalJournal of Engineering for Gas Turbines and Poweren_US
dc.eprint.versionFinal published versionen_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dc.date.updated2018-04-11T12:51:29Z
dspace.orderedauthorsLettieri, Claudio; Paxson, Derek; Spakovszky, Zoltan; Bryanston-Cross, Peteren_US
dspace.embargo.termsNen_US
dc.identifier.orcidhttps://orcid.org/0000-0002-0673-430X
dc.identifier.orcidhttps://orcid.org/0000-0003-2167-9860
mit.licensePUBLISHER_POLICYen_US


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