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 | 74 | 2018 |
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 | 30 | 2021 |
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 | 29 | 2019 |
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 | 26 | 2016 |
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 | 16 | 2022 |
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 | 16 | 2020 |
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 | 16 | 2018 |
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 | 15 | 2017 |
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 | 14 | 2021 |
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 | 14 | 2014 |
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 | 13 | 2016 |
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 | 10 | 2022 |
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 | 10 | 2011 |
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 | 9 | 2021 |
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 | 9 | 2021 |
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 | 8 | 2021 |
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 | 7 | 2008 |
Parametric study of rotor tip squealer geometry on the aerodynamic performance of a high subsonic axial compressor stage J Yang, R Wang, M Zhang, Y Liu Journal of the Brazilian Society of Mechanical Sciences and Engineering 43, 1-13, 2021 | 6 | 2021 |
Time-marching throughflow analysis of centrifugal compressors with boundary conditions based on newton’s method C Yang, J Du, H Zhang, H Wu, Q Tang, J Yang Applied Sciences 12 (13), 6576, 2022 | 5 | 2022 |
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 | 5 | 2021 |