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Acoustic characteristics of a ported shroud turbocompressor operating at design conditions

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Acoustic characteristics of a ported shroud turbocompressor operating at design conditions

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dc.contributor.author Sharma, Sidharath es_ES
dc.contributor.author Broatch, A. es_ES
dc.contributor.author GARCIA TISCAR, JORGE es_ES
dc.contributor.author Allport, John M. es_ES
dc.contributor.author Nickson, Ambrose K. es_ES
dc.date.accessioned 2020-09-12T03:34:18Z
dc.date.available 2020-09-12T03:34:18Z
dc.date.issued 2020-10 es_ES
dc.identifier.issn 1468-0874 es_ES
dc.identifier.uri http://hdl.handle.net/10251/149928
dc.description.abstract [EN] In this article, the acoustic characterisation of a turbocharger compressor with ported shroud design is carried out through the numerical simulation of the system operating under design conditions of maximum isentropic efficiency. While ported shroud compressors have been proposed as a way to control the flow near unstable conditions in order to obtain a more stable operation and enhance deep surge margin, it is often assumed that the behaviour under stable design conditions is characterised by a smooth, non-detached flow that matches an equivalent standard compressor. Furthermore, research is scarce regarding the acoustic effects of the ported shroud addition, especially under the design conditions. To analyse the flow field evolution and its relation with the noise generation, spectral signatures using statistical and scale-resolving turbulence modelling methods are obtained after successfully validating the performance and acoustic predictions of the numerical model with experimental measurements. Propagation of the frequency content through the ducts has been estimated with the aid of pressure decomposition methods to enhance the content coming from the compressor. Expected acoustic phenomena such as `buzz-saw¿ tones, blade passing peaks and broadband noise are correctly identified in the modelled spectrum. Analysis of the flow behaviour in the ported shroud shows rotating structures through the slot that may impact the acoustic and vibration response. Further inspection of the pressure field through modal decomposition confirms the influence of the ported shroud cavity in noise generation and propagation, especially at lower frequencies, suggesting that further research should be carried out on the impact these flow enhancement solutions have on the noise emission of the turbocharger. es_ES
dc.description.sponsorship The project was sponsored and supported by BorgWarner Turbo Systems and the Regional Growth Fund (RGF Grant Award 01.09.07.01/1789C). The authors would like to thank BorgWarner Turbo Systems for permission to publish the results presented in this article. The support of the HPC group at the University of Huddersfield is gratefully acknowledged. 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 (by-nc) es_ES
dc.subject Compressor noise es_ES
dc.subject Large eddy simulation es_ES
dc.subject Modal decomposition es_ES
dc.subject Proper orthogonal decomposition es_ES
dc.subject Noise vibration & harshness es_ES
dc.subject Computational fluid dynamics es_ES
dc.subject.classification INGENIERIA AEROESPACIAL es_ES
dc.subject.classification MAQUINAS Y MOTORES TERMICOS es_ES
dc.title Acoustic characteristics of a ported shroud turbocompressor operating at design conditions es_ES
dc.type Artículo es_ES
dc.identifier.doi 10.1177/1468087418814635 es_ES
dc.relation.projectID info:eu-repo/grantAgreement/RGF//01.09.07.01%2F1789C/ 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 Sharma, S.; Broatch, A.; Garcia Tiscar, J.; Allport, JM.; Nickson, AK. (2020). Acoustic characteristics of a ported shroud turbocompressor operating at design conditions. International Journal of Engine Research. 21(8):1454-1468. https://doi.org/10.1177/1468087418814635 es_ES
dc.description.accrualMethod S es_ES
dc.relation.publisherversion https://doi.org/10.1177/1468087418814635 es_ES
dc.description.upvformatpinicio 1454 es_ES
dc.description.upvformatpfin 1468 es_ES
dc.type.version info:eu-repo/semantics/publishedVersion es_ES
dc.description.volume 21 es_ES
dc.description.issue 8 es_ES
dc.relation.pasarela S\373112 es_ES
dc.contributor.funder BorgWarner Turbo Systems es_ES
dc.contributor.funder Regional Growth Fund, Reino Unido es_ES
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