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dc.contributor.authorAgromayor, Roberto
dc.contributor.authorMüller, Bernhard
dc.contributor.authorNord, Lars O.
dc.date.accessioned2019-09-18T06:37:31Z
dc.date.available2019-09-18T06:37:31Z
dc.date.created2019-09-17T11:32:26Z
dc.date.issued2019
dc.identifier.citationInternational Journal of Turbomachinery, Propulsion and Power. 2019, 4 (3), .nb_NO
dc.identifier.issn2504-186X
dc.identifier.urihttp://hdl.handle.net/11250/2617322
dc.description.abstractAnnular diffusers are frequently used in turbomachinery applications to recover the discharge kinetic energy and increase the total-to-static isentropic efficiency. Despite its strong influence on turbomachinery performance, the diffuser is often neglected during the preliminary design. In this context, a one-dimensional flow model for annular diffusers that accounts for the impact of this component on turbomachinery performance was developed. The model allows use of arbitrary equations of state and to account for the effects of area change, heat transfer, and friction. The mathematical problem is formulated as an implicit system of ordinary differential equations that can be solved when the Mach number in the meridional direction is different than one. The model was verified against a reference case to assess that: (1) the stagnation enthalpy is conserved and (2) the entropy computation is consistent and it was found that the error of the numerical solution was always smaller than the prescribed integration tolerance. In addition, the model was validated against experimental data from the literature, finding that deviation between the predicted and measured pressure recovery coefficients was less than 2% when the best-fit skin friction coefficient is used. Finally, a sensitivity analysis was performed to investigate the influence of several input parameters on diffuser performance, concluding that: (1) the area ratio is not a suitable optimization variable because the pressure recovery coefficient increases asymptotically when this variable tends to infinity, (2) the diffuser should be designed with a positive mean wall cant angle to recover the tangential fraction of kinetic energy, (3) the mean wall cant angle is a critical design variable when the maximum axial length of the diffuser is constrained, and (4) the performance of the diffuser declines when the outlet hub-to-tip ratio of axial turbomachines is increased because the channel height is reduced.nb_NO
dc.description.abstractOne-Dimensional Annular Diffuser Model for Preliminary Turbomachinery Designnb_NO
dc.language.isoengnb_NO
dc.publisherMDPInb_NO
dc.relation.urihttps://doi.org/10.5281/zenodo.2634095
dc.rightsNavngivelse 4.0 Internasjonal*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/deed.no*
dc.titleOne-Dimensional Annular Diffuser Model for Preliminary Turbomachinery Designnb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.description.versionpublishedVersionnb_NO
dc.source.pagenumber26nb_NO
dc.source.volume4nb_NO
dc.source.journalInternational Journal of Turbomachinery, Propulsion and Powernb_NO
dc.source.issue3nb_NO
dc.identifier.doihttp://dx.doi.org/10.3390/ijtpp4030031
dc.identifier.cristin1725548
dc.relation.projectNorges forskningsråd: 257632nb_NO
dc.relation.projectNorges forskningsråd: 255016nb_NO
dc.description.localcode© 2019 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).nb_NO
cristin.unitcode194,64,25,0
cristin.unitnameInstitutt for energi- og prosessteknikk
cristin.ispublishedtrue
cristin.fulltextoriginal
cristin.qualitycode1


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