Analysis of the Influence of Intentional Mistuning on the Forced Response Characteristics of the Splittered Impeller via ROM
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-4010-9_73
Reference29 articles.
1. Cumpsty, N.A.: Compressor Aerodynamics. Krieger Publishing Company, Florida (2004)
2. Xiang, H., Chen, J., Cheng, J., et al.: A novel approach to determine splitter vane length for an extremely high hub/tip ratio mixed-flow compressor impeller. Proc. Inst. Mech. Eng. Part A: J. Power Energy 234(4), 401–419 (2020)
3. Jebieshia, T.R., Raman, S.K., Kim, H.D.: Aerodynamic and structural characteristics of a centrifugal compressor impeller. Appl. Sci. 9(16), 3416 (2019)
4. Bednarz, A., Kabalyk, K., Jakubowski, R., et al.: Numerical study on sensitivity of turbofan engine performance to blade count of centrifugal compressor impeller. Energies 16(14), 5251 (2023)
5. Torre, F., Konno, S., Lettieri, C., et al.: Design optimization of splitter blades for rocket engine turbopump. In: Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, Volume 2D: Turbomachinery, GT2018–75192. Oslo, Norway (2018)
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