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Publishing Language: Chinese

Review and progress of research on blade source term model

Fang ZHOU1, Qingyong WANG1, Yuqi QIN1, Botao ZHANG2, Yangang WANG1( )
School of Power and Energy, Northwestern Polytechnical University, Xi'an 710129, China
Taihang Laboratory, Chengdu 610299, China
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Abstract

With the enhancement of the coupling depth between the distributed propulsion system and the aircraft in terms of structure and aerodynamics, the blade source term model that balances calculation accuracy and efficiency plays an increasingly important role in the analysis and optimization of the internal and external flow coupling of the distributed layout. This paper systematically reviews the basic logic, implementation path and application results of the existing blade source term models for compressors, fans, propellers, etc., and provides support for the selection of blade source term models in the process of internal and external flow coupling analysis of distributed propulsion systems. Firstly, the applications and development of the descriptive and iterative body force methods based on the actuator disk model are reviewed and summarized. The Hough-Ordway model and its improvement ideas are discussed. The potential flow-viscous flow coupling and the iterative calculation strategy based on Blade Element Momentum Theory (BEMT) coupling are analyzed. Secondly, the applications and development of the analysis mode and the extraction mode body force model based on the Marble body force model are sorted out. The Gong model, the Hall model, and the improved Gong-Thollet model and Hall-Thollet model based on the analysis mode are discussed. Subsequently, the body force models of Turbine Engine Analysis Compressor Code (TEACC), Kiwada and Chima, which directly extract the blade source terms from the flow field data by using the streamline curvature method and the Reynolds-Averaged Navier-Stokes (RANS) equation calculation results, are discussed. Finally, the collected blade source term models are compared and analyzed, and specific suggestions for the applications of blade source term models in numerical analysis of rotating turbomachinery are given, which provides a reference for the integrated analysis of internal and external flow for balancing calculation accuracy and efficiency.

CLC number: V231.1 Document code: A Article ID: 1000-6893(2025)10-031178-21

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
ZHOU F, WANG Q, QIN Y, et al. Review and progress of research on blade source term model. Acta Aeronautica et Astronautica Sinica, 2025, 46(10). https://doi.org/10.7527/S1000-6893.2024.31178

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Received: 10 September 2024
Revised: 15 October 2024
Accepted: 05 December 2024
Published: 18 December 2024
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica