Show simple item record

dc.contributor.advisorZoltán S. Spakovszky.en_US
dc.contributor.authorPaxson, Derek Edwinen_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2017-02-22T19:01:20Z
dc.date.available2017-02-22T19:01:20Z
dc.date.copyright2016en_US
dc.date.issued2016en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/107053
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2016.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 149-152).en_US
dc.description.abstractThis thesis is focused on the experimental characterization of the thermodynamic properties and behavior of carbon dioxide (CO₂ ) undergoing non-equilibrium condensation near the critical point in a convergent-divergent nozzle. The insight gained facilitates new modelling tools that guide the design of more efficient compressors for applications such as carbon capture and sequestration (CCS), enhanced oil recovery (EOR), and Supercritical CO₂ power cycles. Modelling of non-equilibrium condensation requires knowledge of the fluid's metastable (subcooled-vapor) properties and related stability limit, known as the Wilson line. While there have been computational studies on metastable CO₂, there is no experimental data in the literature to anchor these results for conditions near the critical point. A laboratory scale blowdown experiment was constructed to visualize the onset of condensation, allowing for a first-of-its-kind assessment of the Wilson line, and the accuracy of two methods for determining metastable properties: spline-based extrapolation and equation of state (EOS) based extrapolation using the Span and Wagner EOS. The experiment consists of a heated charge tank and an optically accessible instrumented convergent-divergent nozzle. The nozzle was sized such that relevant length and time-scales were similar to those of the flow around a compressor leading edge. Pressure transducers were used to provide static pressure data, and a novel shearing interferometer, tailored to the high densities of supercritical CO₂, was developed to measure the static density. The maximum errors between measured and calculated metastable densities are 2%, and 15% for the Span and Wagner EOS and tabular extrapolation methods, respectively. The conditions under which condensation was observed in the experiment were used to establish the Wilson line. Based on this, a new safety limit for compressor inlet conditions near the critical point enabling greater compressor efficiencies was developed.en_US
dc.description.statementofresponsibilityby Derek Edwin Paxson.en_US
dc.format.extent191 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleExperimental characterization of condensation behavior for metastable carbon dioxideen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc971022352en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record