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Turbocharger turbine rotor tip leakage loss and mass flow model valid up to extreme off-design conditions with high blade to jet speed ratio

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Turbocharger turbine rotor tip leakage loss and mass flow model valid up to extreme off-design conditions with high blade to jet speed ratio

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Serrano, J.; Navarro, R.; García-Cuevas González, LM.; Inhestern, LB. (2018). Turbocharger turbine rotor tip leakage loss and mass flow model valid up to extreme off-design conditions with high blade to jet speed ratio. Energy. 147:1299-1310. https://doi.org/10.1016/j.energy.2018.01.083

Por favor, use este identificador para citar o enlazar este ítem: http://hdl.handle.net/10251/122886

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Title: Turbocharger turbine rotor tip leakage loss and mass flow model valid up to extreme off-design conditions with high blade to jet speed ratio
Author: Serrano, J.R. Navarro, Roberto García-Cuevas González, Luis Miguel Inhestern, Lukas Benjamin
UPV Unit: Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics
Issued date:
Abstract:
[EN] Due to the power consumption restriction of the turbocharger compressor, common turbine maps are rather narrow. To extrapolate them, reliable physical submodels are needed that are valid for broad ranges. Plenty of ...[+]
Subjects: Radial turbine model , Tip leakage , Off-design , High BSR , CFD , Wide map
Copyrigths: Reconocimiento - No comercial - Sin obra derivada (by-nc-nd)
Source:
Energy. (issn: 0360-5442 )
DOI: 10.1016/j.energy.2018.01.083
Publisher:
Elsevier
Publisher version: https://doi.org/10.1016/j.energy.2018.01.083
Project ID:
AEI/TRA2016-79185-R
Thanks:
The work has been partially supported by FEDER and the Spanish Ministry of Economy and Competitiveness through grant number TRA2016-79185-R.
Type: Artículo

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