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Turbocharger radial turbine response to pulse shape under realistic operating conditions
KTH, School of Industrial Engineering and Management (ITM), Centres, Competence Center for Gas Exchange (CCGEx). KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0001-7352-0902
KTH, School of Industrial Engineering and Management (ITM), Centres, Competence Center for Gas Exchange (CCGEx). KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0002-6090-1498
KTH, School of Industrial Engineering and Management (ITM), Centres, Competence Center for Gas Exchange (CCGEx). KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0001-7330-6965
2020 (English)In: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020, American Society of Mechanical Engineers (ASME) , 2020Conference paper, Published paper (Refereed)
Abstract [en]

Understanding how energy-conversion mechanisms, i.e. turbine power, heat transfer and total internal irreversibilities are affected by mass flow rate pulse characteristics, i.e. amplitude, frequency and temporal gradient, is a key technological factor to improve turbocharger turbine efficiency under pulsating flow conditions. In this work, the turbocharger turbine response to pulse shape is studied by comparing two different mass flow profiles, characterized by a 5% difference in amplitude, via a Detached Eddy Simulation (DES). With increasing amplitude, an exergy-based post-processing analysis shows a 1.5% increase in turbine power, and the growth of total internal irreversibilities by 7%, 8% and 3% inside the exhaust manifold, volute and turbine, respectively. The Bejan number distribution demonstrates that viscous dissipation, due to higher velocity gradients, is responsible for the increase of total internal irreversibilities. Furthermore, pulse amplitude effect on heat transfer is larger at the exhaust manifold compared to the volute. Under pulsating flow conditions, isentropic efficiency is demonstrated to provide inconsistent results rather than an exergy-based efficiency, which requires no phase correction. The analysis of secondary flows inside the volute highlights the formation of pairs of counter-rotating vortices, which interfere with the correct alignment of velocity triangles by adding a vertical component to the velocity field at the rotor inlet in the direction of the turbine axis of rotation.

Place, publisher, year, edition, pages
American Society of Mechanical Engineers (ASME) , 2020.
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-332037DOI: 10.1115/GT2020-15237Scopus ID: 2-s2.0-85099775540OAI: oai:DiVA.org:kth-332037DiVA, id: diva2:1782985
Conference
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020, Virtual, Online, Sep 25 2020 - Sep 21 2020
Note

Part of ISBN 9780791884102

QC 20230714

Available from: 2023-07-18 Created: 2023-07-18 Last updated: 2025-02-09Bibliographically approved

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Mosca, RobertoLim, Shyang MawMihaescu, Mihai

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