Refined entropy analysis in turbine cascade: A novel loss decomposition method for flow with large separation

To address the deficiency in loss diagnostic methods for turbines working at off-design angles of attack, a novel loss decomposition method suitable for cascade flow with large separation is proposed. The method proposed has the following advantages over existing methods: (A) It enables refined loss decomposition for cascade flows, capable of identifying the spatial range of specific regions such as shear layers and backflow regions, thereby obtaining the loss characteristics of these regions. (B) The region identification criteria in this method have clear physical meanings, rather than relying on arbitrary area division. (C) The method has good applicability and is suitable for cascade flows under various angles of attack. Validation shows that this method achieves satisfactory results. Based on this method, the loss mechanisms of a low-pressure turbine cascade at a low Reynolds number of 4.3 × 10 4 and angles of attack of −5°, −20°, and −45° are investigated using Large Eddy Simulations (LESs). Entropy analysis quantitatively demonstrates significant differences in the composition of losses among flow regions, due to their different flow characteristics. From the perspective of flow regions, wake loss dominates total loss, while loss in backflow region is negligible. Furthermore, the variation mechanisms of loss with incidence differ among different flow regions.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2025-06-21
DOI
https://doi.org/10.1016/j.cja.2025.103644
Primary Topic
Turbomachinery Performance and Optimization
Type
article
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article

Refined entropy analysis in turbine cascade: A novel loss decomposition method for flow with large separation

Dongming Huang, Weihao Zhang, J Wang, Zhengping Zou et al.
Chinese Journal of Aeronautics
Turbomachinery Performance and Optimization
article

Refined entropy analysis in turbine cascade: A novel loss decomposition method for flow with large separation

Dongming Huang, Weihao Zhang, J Wang, Zhengping Zou, Yufan Wang
article en

Abstract

To address the deficiency in loss diagnostic methods for turbines working at off-design angles of attack, a novel loss decomposition method suitable for cascade flow with large separation is proposed. The method proposed has the following advantages over existing methods: (A) It enables refined loss decomposition for cascade flows, capable of identifying the spatial range of specific regions such as shear layers and backflow regions, thereby obtaining the loss characteristics of these regions. (B) The region identification criteria in this method have clear physical meanings, rather than relying on arbitrary area division. (C) The method has good applicability and is suitable for cascade flows under various angles of attack. Validation shows that this method achieves satisfactory results. Based on this method, the loss mechanisms of a low-pressure turbine cascade at a low Reynolds number of 4.3 × 10 4 and angles of attack of −5°, −20°, and −45° are investigated using Large Eddy Simulations (LESs). Entropy analysis quantitatively demonstrates significant differences in the composition of losses among flow regions, due to their different flow characteristics. From the perspective of flow regions, wake loss dominates total loss, while loss in backflow region is negligible. Furthermore, the variation mechanisms of loss with incidence differ among different flow regions.

Chinese Journal of AeronauticsVol. 38(12)
Beihang University (CN)
Affordable and clean energy
Openalex Percentile: Top 81%
Turbomachinery Performance and Optimization
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Refined entropy analysis in turbine cascade: A novel loss decomposition method for flow with large separation — Dongming Huang, Weihao Zhang, et al. · Chinese Journal of Aeronautics (2025) | TGRS Research Map | TGRS