Article Versions Notes

Cheng J, Li B, Song X, Ji X, Zhang Y, Chen J, Xiang H. Integrated Surrogate Model-Based Approach for Aerodynamic Design Optimization of Three-Stage Axial Compressor in Gas Turbine Applications. Energies. 2025; 18(17):4514. https://doi.org/10.3390/en18174514

Cheng, Jinxin, Bin Li, Xiancheng Song, Xinfang Ji, Yong Zhang, Jiang Chen, and Hang Xiang. 2025. "Integrated Surrogate Model-Based Approach for Aerodynamic Design Optimization of Three-Stage Axial Compressor in Gas Turbine Applications" Energies 18, no. 17: 4514. https://doi.org/10.3390/en18174514

Cheng, J., Li, B., Song, X., Ji, X., Zhang, Y., Chen, J., & Xiang, H. (2025). Integrated Surrogate Model-Based Approach for Aerodynamic Design Optimization of Three-Stage Axial Compressor in Gas Turbine Applications. Energies, 18(17), 4514. https://doi.org/10.3390/en18174514