Body Force Modelling of a Multi-Stage High-Pressure Compressor Under Inlet Distortion

The present work aims to propose a new calibration strategy of the Hall–Thollet Body Force (BF) model to simulate the flow in multi-stage compressors and to capture inlet distortion effects within the machine. Both global (0D) and radial (1D) correction terms are introduced and calibrated to improve predictions in multi-stage compressors, accounting for highly interacting, highly loaded blades, falling outside the validity range of the model’s original coefficients. The modified model has been tested on the 3.5-stage high-pressure compressor CREATE, for which experimental data are available. The modified model is then employed to study different patterns of inlet distortion. The results show a very good agreement between Unsteady Reynolds-Averaged Navier–Stokes (URANS) simulations and Body Force calculations in terms of performance, key quantities along the radial and circumferential directions and distortion transfer across the compressor.

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Publication Details

Journal
International Journal of Turbomachinery Propulsion and Power
Published
2025-06-17
DOI
https://doi.org/10.3390/ijtpp10020012
Citations
3
Primary Topic
Refrigeration and Air Conditioning Technologies
Type
article
Field-Weighted Citation Impact
2.14

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article

Body Force Modelling of a Multi-Stage High-Pressure Compressor Under Inlet Distortion

Raphaël Barrier, Guillaume Dufour, Sébastien Cochon, Carmela De Crea et al.
3 citations
International Journal of Turbomachinery Propulsion and Power
Refrigeration and Air Conditioning Technologies
2.14
article

Body Force Modelling of a Multi-Stage High-Pressure Compressor Under Inlet Distortion

Raphaël Barrier, Guillaume Dufour, Sébastien Cochon, Carmela De Crea, Julien Marty
article en
3 citations

Abstract

The present work aims to propose a new calibration strategy of the Hall–Thollet Body Force (BF) model to simulate the flow in multi-stage compressors and to capture inlet distortion effects within the machine. Both global (0D) and radial (1D) correction terms are introduced and calibrated to improve predictions in multi-stage compressors, accounting for highly interacting, highly loaded blades, falling outside the validity range of the model’s original coefficients. The modified model has been tested on the 3.5-stage high-pressure compressor CREATE, for which experimental data are available. The modified model is then employed to study different patterns of inlet distortion. The results show a very good agreement between Unsteady Reynolds-Averaged Navier–Stokes (URANS) simulations and Body Force calculations in terms of performance, key quantities along the radial and circumferential directions and distortion transfer across the compressor.

International Journal of Turbomachinery Propulsion and PowerVol. 10(2)
Université Fédérale de Toulouse Midi-Pyrénées (FR), Institut Superieur de l'Aeronautique et de l'Espace (ISAE-SUPAERO) (FR), Safran (France) (FR)
Association Nationale de la Recherche et de la Technologie, Safran Aircraft Engines
Openalex Percentile: Top 13%
Refrigeration and Air Conditioning Technologies
2.14
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