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Acoustic scattering in a small centrifugal compressor based on the use of linearized equations in a rotating frame
KTH, Skolan för teknikvetenskap (SCI), Teknisk mekanik, Strömningsmekanik och Teknisk Akustik. KTH, Skolan för industriell teknik och management (ITM), Centra, Competence Center for Gas Exchange (CCGEx). Leibniz Institute for Solid State and Materials Research, Helmholzstrasse 4, Dresden, Germany. (CCGEx)ORCID-id: 0000-0001-8456-3924
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
KTH, Skolan för teknikvetenskap (SCI), Teknisk mekanik, Farkostteknik och Solidmekanik.ORCID-id: 0000-0001-7898-8643
2023 (engelsk)Inngår i: Journal of Sound and Vibration, ISSN 0022-460X, E-ISSN 1095-8568, Vol. 544, s. 117315-117315, artikkel-id 117315Artikkel i tidsskrift (Fagfellevurdert) Published
Abstract [en]

Numerical solutions of acoustic wave scattering are often used to describe sound propagation through complex geometries. For cases with flow, various forms of the convected equation have been used. A better alternative that includes vortex-sound interaction is instead to use the linearized and harmonic forms of the unsteady fluid flow governing equations. In this paper, a formulation of the linearized equations that include rotational effects, in an acoustic computation using a rotating frame of reference in a stationary geometry, is presented. We demonstrate that rotational effects can be important, e.g., when computing the transmission loss through high-speed compressors. The implementation of the proposed addition to the existing schemes is both simple and numerically inexpensive. The results are expected to have an impact on the research and development related to noise control of high-performance turbo-machinery, e.g., used in automotive or aviation applications at operating conditions that can be represented by steady background flows.

sted, utgiver, år, opplag, sider
Elsevier, 2023. Vol. 544, s. 117315-117315, artikkel-id 117315
Emneord [en]
Acoustic scattering, compressor noise, linearized equations, experiments
HSV kategori
Forskningsprogram
Teknisk mekanik
Identifikatorer
URN: urn:nbn:se:kth:diva-322073DOI: 10.1016/j.jsv.2022.117315ISI: 000892346700005Scopus ID: 2-s2.0-85141915892OAI: oai:DiVA.org:kth-322073DiVA, id: diva2:1714819
Prosjekter
CCGEx
Forskningsfinansiär
Swedish Energy Agency, 33834-3
Merknad

QC 20230126

Tilgjengelig fra: 2022-11-30 Laget: 2022-11-30 Sist oppdatert: 2025-02-14bibliografisk 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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