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dc.contributor.author | Serrano, J.R. | es_ES |
dc.contributor.author | Arnau Martínez, Francisco José | es_ES |
dc.contributor.author | García-Cuevas González, Luis Miguel | es_ES |
dc.contributor.author | Soler-Blanco, Pablo | es_ES |
dc.contributor.author | Cheung, Raymond | es_ES |
dc.date.accessioned | 2021-02-03T04:33:53Z | |
dc.date.available | 2021-02-03T04:33:53Z | |
dc.date.issued | 2021-02 | es_ES |
dc.identifier.issn | 1468-0874 | es_ES |
dc.identifier.uri | http://hdl.handle.net/10251/160604 | |
dc.description | This is the author¿s version of a work that was accepted for publication in International Journal of Engine Research. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published as https://doi.org/10.1177/1468087419869157 | es_ES |
dc.description.abstract | [EN] This article presents the experimental validation of a complete integrated one-dimensional twin-scroll turbine model able to be used in reciprocating internal combustion engine unsteady simulations. A passenger car with a twin-entry-type turbine has been tested under engine-like pulse conditions by means of a specifically built gas stand. To obtain high-resolution quality data, the turbine and turbine line pipes have been instrumented with mean and instantaneous pressure sensors as well as temperature and mass flow sensors, employing a uniquely designed rotating valve for the pulse generation. This experimental configuration enables to obtain the pressure decomposition in both inlets and outlets of the turbine. Using the experimental data obtained, the model is fully validated, with special focus on the reflected and transmitted components for analysing the performance of the model and its non-linear acoustics prediction capabilities. The model presents a very high degree of correlation with the experimental results, providing a range of errors similar to the uncertainty of the measurements, even in the medium- and high-frequency spectra. | es_ES |
dc.description.sponsorship | The author(s) disclosed receipt of the following financial support for the research, authorship and/or publication of this article: This work was supported by the 'Ayuda a Primeros Proyectos de Investigacion' (PAID-06-18), Vicerrectorado de Investigacion, Innovacion y Transferencia de la Universitat Politecnica de Valencia (UPV), Valencia, Spain. P.S. was partially supported through contract FPI-2017-S2-1428 of Programa de Apoyo para la Investigacion y Desarrollo (PAID) of Universitat Politecnica de Valencia. | es_ES |
dc.language | Inglés | es_ES |
dc.publisher | SAGE Publications | es_ES |
dc.relation.ispartof | International Journal of Engine Research | es_ES |
dc.rights | Reconocimiento - No comercial - Sin obra derivada (by-nc-nd) | es_ES |
dc.subject | Turbocharger | es_ES |
dc.subject | One-dimensional model | es_ES |
dc.subject | Twin turbine | es_ES |
dc.subject | Pulsating flow | es_ES |
dc.subject | Instantaneous turbine performance | es_ES |
dc.subject.classification | MAQUINAS Y MOTORES TERMICOS | es_ES |
dc.subject.classification | INGENIERIA AEROESPACIAL | es_ES |
dc.title | Experimental validation of a one-dimensional twin-entry radial turbine model under non-linear pulse conditions | es_ES |
dc.type | Artículo | es_ES |
dc.identifier.doi | 10.1177/1468087419869157 | es_ES |
dc.relation.projectID | info:eu-repo/grantAgreement/UPV//FPI-2017-S2-1428/ | es_ES |
dc.relation.projectID | info:eu-repo/grantAgreement/UPV//PAID-06-18/ | es_ES |
dc.relation.projectID | info:eu-repo/grantAgreement/UPV//SP20180314/ | es_ES |
dc.rights.accessRights | Abierto | es_ES |
dc.contributor.affiliation | Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics | es_ES |
dc.description.bibliographicCitation | Serrano, J.; Arnau Martínez, FJ.; García-Cuevas González, LM.; Soler-Blanco, P.; Cheung, R. (2021). Experimental validation of a one-dimensional twin-entry radial turbine model under non-linear pulse conditions. International Journal of Engine Research. 22(2):390-406. https://doi.org/10.1177/1468087419869157 | es_ES |
dc.description.accrualMethod | S | es_ES |
dc.relation.publisherversion | https://doi.org/10.1177/1468087419869157 | es_ES |
dc.description.upvformatpinicio | 390 | es_ES |
dc.description.upvformatpfin | 406 | es_ES |
dc.type.version | info:eu-repo/semantics/publishedVersion | es_ES |
dc.description.volume | 22 | es_ES |
dc.description.issue | 2 | es_ES |
dc.relation.pasarela | S\392679 | es_ES |
dc.contributor.funder | Universitat Politècnica de València | es_ES |
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