An Overview of the Benchmark Case for the Aeroacoustics and Structural Acoustics of an Enclosed Centrifugal Fan

As part of a joint research project between the Institute of Fluid Mechanics (LSTM) and the Institute of Fundamentals and Theory of Electrical Engineering (IGTE), an international benchmark case for fluid–structure–acoustic interaction was developed. The research focused on an enclosed centrifugal fan, and its aerodynamic, aeroacoustic and structure–acoustic properties were characterised through experimental measurements. This paper provides an overview of the centrifugal fan, its enclosure and the test rig used for the experimental investigations. Rather than interpreting the results, the focus is on presenting the benchmark case and providing an overview of the available data. The entire benchmark dataset is listed and freely accessible via the Zenodo European platform in the EAA benchmark data collection.

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Publication Details

Journal
International Journal of Turbomachinery Propulsion and Power
Published
2026-02-03
DOI
https://doi.org/10.3390/ijtpp11010010
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
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article

An Overview of the Benchmark Case for the Aeroacoustics and Structural Acoustics of an Enclosed Centrifugal Fan

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International Journal of Turbomachinery Propulsion and Power
Aerodynamics and Acoustics in Jet Flows
article

An Overview of the Benchmark Case for the Aeroacoustics and Structural Acoustics of an Enclosed Centrifugal Fan

Patrick Heidegger, Christoph Heigl, Marco Fritzsche, Manfred Kaltenbacher, Manuel Zaragoza Lauber, Felix Czwielong, Stefan Schoder, Andreas Wurzinger, Stefan Becker
article en

Abstract

As part of a joint research project between the Institute of Fluid Mechanics (LSTM) and the Institute of Fundamentals and Theory of Electrical Engineering (IGTE), an international benchmark case for fluid–structure–acoustic interaction was developed. The research focused on an enclosed centrifugal fan, and its aerodynamic, aeroacoustic and structure–acoustic properties were characterised through experimental measurements. This paper provides an overview of the centrifugal fan, its enclosure and the test rig used for the experimental investigations. Rather than interpreting the results, the focus is on presenting the benchmark case and providing an overview of the available data. The entire benchmark dataset is listed and freely accessible via the Zenodo European platform in the EAA benchmark data collection.

International Journal of Turbomachinery Propulsion and PowerVol. 11(1)
Friedrich-Alexander-Universität Erlangen-Nürnberg (DE), Graz University of Technology (AT), Polytec (Germany) (DE)
Industry, innovation and infrastructure
Openalex Percentile: Top 69%
Aerodynamics and Acoustics in Jet Flows
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