关注
Zhaohua Sheng
Zhaohua Sheng
其他姓名Zhao-Hua Sheng
在 pku.edu.cn 的电子邮件经过验证
标题
引用次数
引用次数
年份
Effects of supersonic nozzle guide vanes on the performance and flow structures of a rotating detonation combustor
D Shen, M Cheng, K Wu, Z Sheng, J Wang
Acta Astronautica 193, 90-99, 2022
722022
Investigation of counter-rotating shock wave and wave direction control of hollow rotating detonation engine with Laval nozzle
G Rong, M Cheng, Z Sheng, X Liu, Y Zhang, J Wang
Physics of Fluids 34 (5), 2022
582022
Unsteady conjugate heat transfer simulation of wall heat loads for rotating detonation combustor
Y Hou, M Cheng, Z Sheng, J Wang
International Journal of Heat and Mass Transfer 221, 125081, 2024
432024
Multi-wave effects on stability and performance in rotating detonation combustors
Z Sheng, M Cheng, JP Wang
Physics of Fluids 35 (7), 2023
372023
Numerical investigation of pre-detonator in rotating detonation engine
ZJ Xia, ZH Sheng, DW Shen, JP Wang
International Journal of Hydrogen Energy 46 (61), 31428-31438, 2021
312021
Experimental research on the performance of hollow and annular rotating detonation engines with nozzles
Y Zhang, Z Sheng, G Rong, D Shen, K Wu, J Wang
Applied Thermal Engineering 218, 119339, 2023
212023
Investigation of counter-rotating shock wave phenomenon and instability mechanisms of rotating detonation engine with hollow combustor and Laval nozzle
G Rong, M Cheng, Z Sheng, X Liu, J Wang
International Journal of Hydrogen Energy 47 (54), 23019-23037, 2022
162022
The behavior of the propagating velocity of rotating detonation waves and counter-rotating shock waves in a hollow combustor
G Rong, M Cheng, Z Sheng, X Liu, Y Zhang, J Wang
Acta Astronautica 200, 371-387, 2022
152022
Spinning pulsed detonation in rotating detonation engine
D Shen, JZ Ma, Z Sheng, G Rong, K Wu, Y Zhang, J Wang
Aerospace Science and Technology 126, 107661, 2022
122022
An active direction control method in rotating detonation combustor
Z Sheng, M Cheng, D Shen, JP Wang
International Journal of Hydrogen Energy 47 (55), 23427-23443, 2022
122022
The influence of plug nozzle and Laval nozzle on the flow field and performance of non-premixed rotating detonation combustor
Y Zhang, M Cheng, X Liu, G Rong, Z Sheng, D Shen, K Wu, J Wang
Physics of Fluids 36 (5), 2024
102024
Investigation of flow field characteristics and performance of carbon–hydrogen/oxygen-rich air rotating detonation engine
G Rong, M Cheng, Y Zhang, Z Sheng, J Wang
Physics of Fluids 35 (9), 2023
72023
Flow field characteristics and particle path tracking of a hollow rotating detonation engine with a Laval nozzle
G Rong, M Cheng, Z Sheng, Y Zhang, X Liu, J Wang
Physics of Fluids 35 (5), 2023
62023
Predicting combustion behavior in rotating detonation engines using an interpretable deep learning method
D Shen, Z Sheng, Y Zhang, G Rong, K Wu, J Wang
Physics of Fluids 35 (7), 2023
32023
BYCFoam: An improved solver for rotating detonation engines based on OpenFOAM
M Cheng, Z Sheng, JP Wang
Energies 17 (4), 769, 2024
22024
Analysis on propulsive performance of hollow rotating detonation engine with Laval nozzle
Y Zhang, JZ Ma, K Wu, M Cheng, Z Sheng, G Rong, D Shen, J Wang, ...
Journal of Propulsion and Power 39 (5), 765-779, 2023
22023
Effects of film cooling injection inclination angle on cooling performance in rotating detonation combustors
D Shen, M Cheng, G Rong, Z Sheng, Y Zhang, J Wang
Physics of Fluids 36 (2), 2024
12024
Propagation of rotating detonation wave with wall-detached injection in a hollow combustor
Y Li, M Cheng, Z Sheng, Y Wang, X Liu, J Wang
International Journal of Hydrogen Energy 49, 1100-1111, 2024
12024
Experimental research on the Performance of Hollow and Annular Rotating Detonation Engines
Y Zhang, JZ Ma, Z Sheng, G Rong, D Shen, J Wang, K Wu
AIAA SCITECH 2023 Forum, 1105, 2023
2023
Numerical study on the unsteady rotating detonation flow-field interacted with turbine guide vane
D Shen, M Cheng, K Wu, Z Sheng, J Wang
系统目前无法执行此操作,请稍后再试。
文章 1–20