Multi-Fidelity Simulation of Gas Turbine Overall Performance by Directly Coupling High-Fidelity Models of Multiple Rotating Components
Author:
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s11630-024-1975-3.pdf
Reference41 articles.
1. Zheng X., Zeng H., Wang B., et al., Numerical simulation method of surge experiments on gas turbine engines. Chinese Journal of Aeronautics, 2023, 36(3): 107–120.
2. Yue K., Cheng L., Zhang T., et al., Numerical simulation of the aerodynamic influence of an aircraft on the hose-refueling system during aerial refueling operations. Aerospace Science and Technology, 2016, 49: 34–40.
3. Tang T., Liu B., The genetic algorithm-radial basis function neural network to quickly predict aerodynamic performance of compressors. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 235(5): 537–552.
4. Yang C., Wu H., Du J., et al., Full-engine simulation of micro gas turbine based on time-marching throughflow method. Applied Thermal Engineering, 2022, 217: 119213.
5. Xu Y., Yan C., Piao Y., Analysis of discrepancies between 3-D coupled and uncoupled schemes based on CFD in full engine simulation. Aerospace Science and Technology, 2022, 131: 107978.
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