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Turbulence Model Impact on Predicting Precursors to Surge Flow Instabilities in a Turbocharger Compressor
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.
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
2022 (English)In: ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition / [ed] ASME, ASME International , 2022, Vol. 10D, p. 12-, article id GT2022-83103Conference paper, Published paper (Refereed)
Abstract [en]

Turbocharger compressor simulations can improve the development of compressors with broad operating ranges and improved noise signatures. At low mass flow rates aerodynamic instabilities, known as rotating stall and surge, limit the operating range of the compressor. However, the triggering factors for these instabilities are currently unknown. High quality numerical methods are therefore needed to capture instabilities and to simulate reliable performance maps. The aim of this study is to improve the understanding of the chosen numerical approach going from design to off-design operating conditions. It is shown that flow structures are under-predicted using URANS k-ω SST and that a LES WALE method better captures the flow structures in the blade region. Further, the level of fluctuations in different parts of the compressor is presented. By increasing the predictive quality of the numerical simulations, the need for empirical calibration can be reduced and turbocharger matching can be improved.

Place, publisher, year, edition, pages
ASME International , 2022. Vol. 10D, p. 12-, article id GT2022-83103
Keywords [en]
URANS, LES, Flow Instabilities, Turbocharger compressor, Precursor to surge
National Category
Fluid Mechanics Vehicle and Aerospace Engineering Mechanical Engineering
Research subject
Engineering Mechanics; Vehicle and Maritime Engineering
Identifiers
URN: urn:nbn:se:kth:diva-328408DOI: 10.1115/GT2022-83103Scopus ID: 2-s2.0-85141706199OAI: oai:DiVA.org:kth-328408DiVA, id: diva2:1764692
Conference
ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, Rotterdam, The Netherlands, June 13 – 17, 2022
Projects
CCGEx
Funder
Swedish Energy Agency, 33834-3
Note

QC 20230614

Available from: 2023-06-09 Created: 2023-06-09 Last updated: 2025-02-14Bibliographically approved
In thesis
1. Operating conditions impact on flow and acoustics in turbocharger compressors
Open this publication in new window or tab >>Operating conditions impact on flow and acoustics in turbocharger compressors
2023 (English)Doctoral thesis, comprehensive summary (Other academic)
Abstract [en]

Fluid machines are an integral part in energy conversion with applications from pumps, fans, propellers, compressors and turbines. In the automotive industry, turbochargers are commonly employed to counteract the effect of engine downsizing. However, designing efficient compressors with wide operating ranges and reduced noise emissions consitute a challenge.

This thesis investigates flow instabilities and sound generation in turbocharger compressors, utilizing compressible Large Eddy Simulations (LES). The numerical approach is validated through sensitivity studies and comparison with measurement data. Three different compressor designs used in both light-duty and heavy-duty applications are examined with the aim of enhancing the understanding of rotating stall mechanism in real-world configurations and their impact on aerodynamically generated noise.

The analysis employs compressible Navier-Stokes equations with a scale-resolving model, evaluating its robustness in comparison to other computational methods under various operating conditions. The system's response to time-varying boundary conditions is assessed, and the effect of pulse amplitude is quantified.

Subsequently, the mechanism for aerodynamically generated noise, focusing on the broadband components are explored through analysis of the recirculation region. Resolving the Taylor micro-scale in the recirculation region enhances the understanding of the dynamics in this zone. It is demonstrated that an inlet recirculation zone develops near surge conditions, which is highly sensitive to the choice of boundary conditions and turbulence formulation. Passive flow control, such as the ported-shroud, are considered to illustrate their influence on performance, stability and noise.

Finally, the system is studied using a two-port method, accounting for rotational effects. This provide insights into the transmission poperties at low frequencies (< 3 kHz) and the mechanism of sound generation. It is demonstrated that the use of Computational Fluid Dynamics can improve the understanding of flow-acoustic interaction in complex geometries. Additionally, the developed numerical simulation and post-processing methods have potential application in a range of turbochargr systems, from hybrids to fuel cell application.

Place, publisher, year, edition, pages
Stockholm: KTH Royal Institute of Technology, 2023
Series
TRITA-SCI-FOU ; 2023:58
Keywords
Turbocharger, compressor, LES, surge, rotating stall, flow instabilities, inlet recirculation, aeroacoustics, acoustics
National Category
Engineering and Technology Fluid Mechanics
Research subject
Engineering Mechanics
Identifiers
urn:nbn:se:kth:diva-339638 (URN)978-91-8040-775-5 (ISBN)
Public defence
2023-12-06, F3, Lindstedtsvägen 26, Stockholm, 10:00 (English)
Opponent
Supervisors
Funder
Swedish Energy Agency, 33834-3
Available from: 2023-11-16 Created: 2023-11-15 Last updated: 2025-02-09Bibliographically approved

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Publisher's full textScopushttps://doi.org/10.1115/GT2022-83103

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Trigell, EmelieMihaescu, Mihai

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