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Jinguang Yang
Jinguang Yang
Bestätigte E-Mail-Adresse bei dlut.edu.cn
Titel
Zitiert von
Zitiert von
Jahr
Aerodynamic design optimization of radial-inflow turbine in supercritical CO2 cycles using a one-dimensional model
G Lv, J Yang, W Shao, X Wang
Energy conversion and management 165, 827-839, 2018
742018
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model
C Yang, H Wu, J Yang, M Ferlauto
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
272019
Design parameters exploration for supercritical CO2 centrifugal compressors under multiple constraints
W Shao, X Wang, J Yang, H Liu, Z Huang
Turbo Expo: Power for Land, Sea, and Air 49873, V009T36A008, 2016
262016
Accuracy study and stability control of a property-table-based CFD strategy for modeling SCO2 compressors working near the critical point of the fluid
W Shao, J Yang, X Wang, Z Ma
Applied Thermal Engineering 183, 116222, 2021
232021
A symmetrical-nonuniform angular repartition strategy for the vane blades to improve the energy conversion ability of the coolant pump in the pressurized water reactor
Y Lu, J Yang, X Wang, F Zhou
Nuclear Engineering and Design 337, 245-260, 2018
152018
A real gas-based throughflow method for the analysis of SCO2 centrifugal compressors
W Shao, J Yang, X Wang, Z Ma
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2020
142020
An improved steady inverse method for turbomachinery aerodynamic design
J Yang, Y Liu, X Wang, H Wu
Inverse Problems in Science and Engineering 25 (5), 633-651, 2017
142017
Numerical Analysis of Labyrinth Seal Performance for the Impeller Backface Cavity of a Supercritical CO2 Radial In flow Turbine
J Yang, F Zhao, M Zhang, Y Liu, X Wang
Computer Modeling in Engineering & Sciences 126 (3), 935-953, 2021
132021
The effect of impeller–diffuser interactions on diffuser performance in a centrifugal compressor
PF Zhao, Y Liu, HK Li, XF Wang, JG Yang
Engineering Applications of Computational Fluid Mechanics 10 (1), 565-577, 2016
122016
Explicit coupled solution of two-equation k-ω SST turbulence model and its application in turbomachinery flow simulation
JG Yang, H Wu
Acta Aeronautica et Astronautica Sinica 35 (1), 2014
112014
Investigation on One-Dimensional Loss Models for Predicting Performance of Multistage Centrifugal Compressors in Supercritical CO2 Brayton Cycle
W Shao, J Du, J Yang, X Wang, G Lyu
Journal of Thermal Science 30, 133-148, 2021
102021
Multi-row inverse method based on the adjoint optimization
J Yang, X Huang, H Wu
Turbo Expo: Power for Land, Sea, and Air 54679, 1323-1333, 2011
102011
Full-engine simulation of micro gas turbine based on time-marching throughflow method
C Yang, H Wu, J Du, H Zhang, J Yang
Applied Thermal Engineering 217, 119213, 2022
92022
Aeroacoustic optimization of the bionic leading edge of a typical blade for performance improvement
H Liu, Y Lu, J Yang, X Wang, J Ju, J Tu, Z Yang, H Wang, X Lai
Machines 9 (8), 175, 2021
82021
Improved streamline curvature throughflow method and its application in a bypass compression system design
S Fu-yong, Y Jin-guang, LIU Zhen-de, HU Jun
航空动力学报 23 (6), 1072-1076, 2008
72008
Experimental Study on the Density-Driven Convective Mixing of CO2 and Brine at Reservoir Temperature and Pressure Conditions
L Jiang, Y Wang, G Lu, J Yang, Y Song
Energy & Fuels 36 (17), 10261-10268, 2022
62022
Stator re-stagger optimization in multistage axial compressor
J Yang, M Zhang, C Peng, M Ferlauto, Y Liu
Propulsion and Power Research 10 (2), 107-117, 2021
62021
A novel preliminary design method for intermediate compressor/turbine ducts
J Yang, Y Liu, N Wu, M Zhang, W Shao, Y Liu
Aerospace Science and Technology 117, 106974, 2021
52021
Numerical simulations and optimizations for turbine-related configurations
J Yang, M Zhang, Y Liu
Thermal Science 24 (1 Part A), 367-378, 2020
52020
3D viscous inverse design of turbomachinery using one-equation turbulence model
J Yang, Y Liu, X Wang, H Wu
Turbo Expo: Power for Land, Sea, and Air 49712, V02CT39A014, 2016
52016
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