Author:
Cheng Jinxin,Zhang Yong,Chen Jiang,Ma Hui,Liu Beiying
Funder
Fundamental Research Funds for the Central Universities
National Natural Science Foundation of China
Basic and Applied Basic Research Foundation of Guangdong Province
Reference36 articles.
1. Experimental mode decomposition investigation on 3-stage axial flow compressor stall phenomena using aeroacoustics measurements;Guan;Aerosp. Sci. Technol.,2023
2. Effects of the foam metal casing treatment on aerodynamic stability and aerocoustic noise in an axial flow compressor;Sun;Aerosp. Sci. Technol.,2021
3. Survey of modeling and optimization strategies to solve high-dimensional design problems with computationally-expensive black-box functions;Shan;Struct. Multidiscip. Optim.,2010
4. A surface parametric control and global optimization method for axial flow compressor blades;Cheng;Chin. J. Aeronaut.,2019
5. C.J. Brooks, A.I.J. Forrester, A.J. Keane, et al., Multi-fidelity design optimisation of a transonic compressor rotor[C]. 9th European Conf. Turbomachinery Fluid Dynamics and Thermodynamics, Istanbul, Turkey. 21–25 Mar 2011. 10 pp.