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.
Authors
- Raphaël Barrier
- Guillaume Dufour (ORCID: https://orcid.org/0000-0001-6335-1850)
- Sébastien Cochon
- Carmela De Crea (ORCID: https://orcid.org/0000-0002-7303-9657)
- Julien Marty
Institutions
- Université Fédérale de Toulouse Midi-Pyrénées (FR)
- Institut Superieur de l'Aeronautique et de l'Espace (ISAE-SUPAERO) (FR)
- Safran (France) (FR)
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
Funders
- Association Nationale de la Recherche et de la Technologie
- Safran Aircraft Engines