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Hefang Deng
Hefang Deng
Подтвержден адрес электронной почты в домене sjtu.edu.cn
Название
Процитировано
Процитировано
Год
Overall cooling performance evaluation for film cooling with different winglet pairs vortex generators
H Deng, J Teng, M Zhu, X Qiang, S Lu, Y Jiang
Applied Thermal Engineering 201, 117731, 2022
342022
Effects of moving endwall on the unsteadiness of tip leakage flow in compressor cascades
X Qiang, H Deng, K Xia, J Teng, M Zhu, S Lu
Physics of Fluids 35 (8), 2023
172023
Investigation on the inflow distortion of a propulsive fuselage aircraft and its impact on the propulsion fan performance
H Deng, K Xia, X Qiang, M Zhu, J Teng, H Li
Physics of Fluids 35 (5), 2023
102023
Loss analysis of cavity leakage flow in a compressor cascade
H Deng, K Xia, J Teng, S Lu, M Zhu, X Qiang
Journal of Turbomachinery 144 (12), 121008, 2022
72022
Numerical investigation on film cooling mechanism with different coolant delivery configurations
YT Jiang, HF Deng, XL You, HJ Zhao, GQ Yue
Journal of Applied Fluid Mechanics 14 (1), 175-185, 2020
52020
Overall performance and loss analysis of a low-speed research compressor with different nonaxisymmetric tip clearance layouts
K Xia, H Deng, H Zhang, M Zhu, X Qiang, J Teng
Journal of Aerospace Engineering 36 (5), 04023055, 2023
32023
An experimental facility with the high-speed moving endwall for axial compressor leakage flow research
H Deng, K Xia, J Teng, X Qiang, M Zhu, S Lu
Aerospace 10 (3), 226, 2023
32023
Impact of non-axisymmetric tip clearance on the aerodynamic and aeroelastic stabilities of a transonic compressor
K Xia, H Chen, H Deng, M Zhu, X Qiang, J Teng
Aerospace Science and Technology 153, 109457, 2024
22024
Performance prediction and design optimization of a transonic rotor based on deep transfer learning
H Deng, S Zhang, K Xia, X Qiang, M Zhu, J Teng
Physics of Fluids 36 (9), 2024
22024
Analysis of leakage flow and loss in a linear compressor cascade with moving endwall
H Deng, K Xia, J Teng, X Qiang, M Zhu, S Lu
Aerospace Systems 6 (1), 107-118, 2023
22023
Unsteady flow phenomenon in the TUDa-GLR-OpenStage compressor: URANS observations
H Deng, X He, M Zhu, F Klausmann, J Teng
GPPS Conference Hong Kong, GPPS-TC-2023-002, 2023
22023
Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall
K Xia, H Deng, S Lu, J Teng, X Qiang, M Zhu
International Journal of Turbo & Jet-Engines 41 (2), 363-375, 2024
12024
The impact of second-harmonic tip clearance distributions caused by casing Ovalization and blade height variation in a large-scale compressor stage
K Xia, H Deng, Y Zhong, M Zhu, X Qiang, J Teng
Aerospace Science and Technology 145, 108866, 2024
12024
Numerical Research on Near Stall Characteristics of a Transonic Axial Compressor Based on Wavelet Analysis
K Xia, J Feng, M Zhu, H Deng, X Qiang, J Teng
Turbo Expo: Power for Land, Sea, and Air 86090, V10AT29A029, 2022
12022
Investigation of aeroelastic instability in a transonic compressor with low engine order distortion
H Chen, K Xia, H Deng, M Zhu, J Teng
Aerospace Science and Technology 159, 109953, 2025
2025
On the Mechanism of Rotating Stall in a Boundary Layer Ingesting Fan
H Deng, S Zhang, KL Xia, X Qiang, M Zhu, J Teng
Journal of Engineering for Gas Turbines and Power, 1-42, 2025
2025
Performance Effect of Trench Casing on a Transonic Compressor at Different Rotating Speeds
H Deng, K Xia, J Teng, X Qiang, M Zhu, S Lu
Journal of Shanghai Jiaotong University (Science) 29 (6), 1151-1160, 2024
2024
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor
H Deng, K Xia, X Qiang, M Zhu, J Teng, S Lu
International Journal of Turbo & Jet-Engines, 2024
2024
Effects of blade loading distribution on hub leakage flow of cantilevered stator
Y Liu, SJ Tong, H Deng, J Teng, M Zhu, S Zhang, S Lu
2024
Inlet distortion of a rear engines concept aircraft and its effect on a fan
X Qiang, Y Xue, H Deng
Case Studies in Thermal Engineering 61, 105032, 2024
2024
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Статьи 1–20