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Heli Yang
Heli Yang
Verified email at tsinghua.edu.cn
Title
Cited by
Cited by
Year
End-wall boundary layers and blockages of multistage axial compressors under different conditions
X Zheng, H Yang
Journal of Propulsion and Power 33 (4), 908-916, 2017
222017
Compressor geometric uncertainty quantification under conditions from near choke to near stall
W Junying, W Baotong, Y Heli, SUN Zhenzhong, Z Kai, X Zheng
Chinese Journal of Aeronautics 36 (3), 16-29, 2023
112023
Influence of tip clearance on the performance and matching of multistage axial compressors
X Zheng, H Yang
Turbo Expo: Power for Land, Sea, and Air 49699, V02AT37A008, 2016
92016
Numerical simulation method of surge experiments on gas turbine engines
X Zheng, Z Hanxuan, W Baotong, WEN Mengyang, Y Heli, ...
Chinese Journal of Aeronautics 36 (3), 107-120, 2023
72023
Rapid performance prediction model of axial turbine with coupling one-dimensional inverse design and direct analysis
B Wang, Z Song, W Zou, H Yang, M Wen, K Zhou, X Feng, X Zheng
Aerospace Science and Technology 130, 107828, 2022
62022
Investigation on probe streamwise distribution for surge measurement in compression system
J Li, B Wang, H Yang, T Fan, Z Song, J Wang, X Zheng
Aerospace Science and Technology 131, 108009, 2022
32022
An efficient quantification method based on feature selection for high-dimensional uncertainties of multistage compressors
J Wang, X Zheng, H Yang, Z Sun, Z Song, Y Fu
Journal of Engineering for Gas Turbines and Power 145 (2), 021002, 2023
22023
Performance dispersion control of a multistage compressor based on precise identification of critical features
J Wang, H Yang, K Zhou, J Wei, M Wen, X Zheng
Aerospace Science and Technology 129, 107845, 2022
22022
Transient Tip Clearance Prediction Model Considering Transient Radial Temperature Distribution of Discs in a Gas Turbine Engine
J Wei, H Yang, P Zheng, B Wang, X Zheng
Turbo Expo: Power for Land, Sea, and Air 87059, V11AT22A027, 2023
12023
Transient Tip Clearance Prediction Model Considering Transient Radial Temperature Distribution of Discs in a Gas Turbine Engine
J Wei, H Yang, P Zheng, B Wang, X Zheng
Journal of Turbomachinery 146 (4), 2024
2024
Investigation of endwall treatment and shock control in a five-stage axial compressor
H Yang, X Zheng
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2020
2020
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