APA (7th ed.) Citation

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 (19961073), 18(17), 4514. https://doi.org/10.3390/en18174514

Chicago Style (17th ed.) Citation

Cheng, Jinxin, Bin Li, Xiancheng Song, Xinfang Ji, Yong Zhang, Jiang Chen, and Hang Xiang. "Integrated Surrogate Model-Based Approach for Aerodynamic Design Optimization of Three-Stage Axial Compressor in Gas Turbine Applications." Energies (19961073) 18, no. 17 (2025): 4514. https://doi.org/10.3390/en18174514.

MLA (9th ed.) Citation

Cheng, Jinxin, et al. "Integrated Surrogate Model-Based Approach for Aerodynamic Design Optimization of Three-Stage Axial Compressor in Gas Turbine Applications." Energies (19961073), vol. 18, no. 17, 2025, p. 4514, https://doi.org/10.3390/en18174514.