Effects of Swirl Distortion on Flow Field and Blade Load of a Centrifugal Compressor
Author:
Affiliation:
1. School of Intelligent Manufacturing , Weifang University of Science and Technology , Shouguang , Shandong , , China .
2. School of Mechanical and Equipment Engineering , Hebei University of Engineering , Handan , Hebei , , China .
Abstract
Publisher
Walter de Gruyter GmbH
Link
https://www.sciendo.com/pdf/10.2478/amns-2024-1078
Reference18 articles.
1. Ariga, I., Kasai, N., Masuda, S., Watanabe, Y., & Watanabe, I. (1983). The effect of inlet distortion on the performance characteristics of a centrifugal compressor. Journal of engineering for power, 105(2), 223-230.
2. Qiao, W. Y., & Cai, Y. H. (2001). Numerical modeling of the unsteady aerodynamic loads in axial flow compressor with inlet distortions. JOURNAL OF PROPULSION TECHNOLOGY-BEIJING-, 22(5; ISSU 119), 392-396.
3. Zemp, A., Kammerer, A., & Abhari, R. S. (2008, January). Unsteady CFD investigation on inlet distortion in a centrifugal compressor. In ASME Turbo Expo 2008: Power for Land, Sea, and Air (pp. 1909-1919). American Society of Mechanical Engineers.
4. Kammerer, A., & Abhari, R. S. (2010). Blade forcing function and aerodynamic work measurements in a high speed centrifugal compressor with inlet distortion. Journal of Engineering for Gas Turbines and Power, 132(9), 092504.
5. Kim, Y., Engeda, A., Aungier, R., & Direnzi, G. (2001). The influence of inlet flow distortion on the performance of a centrifugal compressor and the development of an improved inlet using numerical simulations. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 215(3), 323-338.
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