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Dynamics of the inlet recirculation region in a turbocharger compressor
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0001-7330-6965
CMT - Clean Mobility & Thermofluids, Universitat Politecnica de Valencia.
CMT - Clean Mobility & Thermofluids, Universitat Politecnica de Valencia.
(English)Manuscript (preprint) (Other academic)
Abstract [en]

A numerical study is presented where Large Eddy Simulation (LES) calculations are used in an effort to characterise flow-acoustic interaction in a turbocharger compressor operating at near surge conditions. Under such off-design operation, an inlet recirculation zone develops upstream of the compressor following the compressor inlet duct. Previous studies have shown that the development of reversed flow can impact the sound power level of the blade passing frequency (BPF) tones and broadban whoosh noise. In this study local mesh independence studies are performed to capture the vortical structures in the recirculation region, which are often not properly resolved. Computational grid refinements in the fluid domain are applied based on extimated of the local Taylor microscale in the flow. Moreover, the grid resolution is enhanced in the region where domainant acoustic sources are to be expected according to Proadman noise source model. The temperature field and the velocity components with correponding standard deviations are quantified and validated against avaliable experimental data. The analysis of the LES data allows quantifying the dynamics of the developed recirculation zone in space and time and enables a detailed assessment on the impact it has on the incoming flow, explaining its contribution to the flow-induced noise mechanisms in a centrifugal compressor.

National Category
Fluid Mechanics
Research subject
Engineering Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-339649OAI: oai:DiVA.org:kth-339649DiVA, id: diva2:1812371
Funder
Swedish Energy Agency, 33834-3
Note

QC 20231120

Available from: 2023-11-15 Created: 2023-11-15 Last updated: 2025-02-09Bibliographically 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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Trigell, EmelieMihaescu, Mihai

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