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Large eddy simulations of a turbocharger compressor under pulsating backpressure conditions
KTH, Skolan för teknikvetenskap (SCI), Teknisk mekanik, Strömningsmekanik och Teknisk Akustik.
KTH, Skolan för teknikvetenskap (SCI), Teknisk mekanik, Strömningsmekanik och Teknisk Akustik.ORCID-id: 0000-0001-7330-6965
(engelsk)Manuskript (preprint) (Annet vitenskapelig)
Abstract [en]

This numerical study focuses on using Large Eddy Simulations to investigate the influence of pulsating backpressure on turbocharger compressor performance, stability and noise generation. This to simulate the effects of the valve train. The study investigates how pulsating backpressure effects compressor performance, especially in the design and near surge conditions. Previous research has indicated that compressor performance deviated from continuous operation under pulsating conditions, resulting in a hysteresis loop. Additionally, the surge margin is affected due to time-history effects. The study employs a pulsating frequency of 100 Hz and examines the sensitivity to pulse amplitude. These results contribute to an improved understainding of the impact of pulsating backpressure on compressor performance and stability, quantifying the effects and providing valuable insights.

HSV kategori
Forskningsprogram
Teknisk mekanik
Identifikatorer
URN: urn:nbn:se:kth:diva-339648OAI: oai:DiVA.org:kth-339648DiVA, id: diva2:1812363
Forskningsfinansiär
Swedish Energy Agency, 33834-3
Merknad

QC 20231120

Tilgjengelig fra: 2023-11-15 Laget: 2023-11-15 Sist oppdatert: 2025-02-09bibliografisk kontrollert
Inngår i avhandling
1. Operating conditions impact on flow and acoustics in turbocharger compressors
Åpne denne publikasjonen i ny fane eller vindu >>Operating conditions impact on flow and acoustics in turbocharger compressors
2023 (engelsk)Doktoravhandling, med artikler (Annet vitenskapelig)
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.

sted, utgiver, år, opplag, sider
Stockholm: KTH Royal Institute of Technology, 2023
Serie
TRITA-SCI-FOU ; 2023:58
Emneord
Turbocharger, compressor, LES, surge, rotating stall, flow instabilities, inlet recirculation, aeroacoustics, acoustics
HSV kategori
Forskningsprogram
Teknisk mekanik
Identifikatorer
urn:nbn:se:kth:diva-339638 (URN)978-91-8040-775-5 (ISBN)
Disputas
2023-12-06, F3, Lindstedtsvägen 26, Stockholm, 10:00 (engelsk)
Opponent
Veileder
Forskningsfinansiär
Swedish Energy Agency, 33834-3
Tilgjengelig fra: 2023-11-16 Laget: 2023-11-15 Sist oppdatert: 2025-02-09bibliografisk kontrollert

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