Jingjun Zhong

Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number

Huawei Lu, Yi Yang, Shuang Guo et al. · Aerospace Science and Technology · 2018 · 51 citations

Engineering, Aerospace Engineering, Aerodynamics +13

Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor

Shaobing Han, Jingjun Zhong · Chinese Journal of Aeronautics · 2016 · 42 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +16

Numerical study on endwall fence with varying geometrical parameters in a highly-loaded compressor cascade

Yunzhi Chen, Ling Yang, Jingjun Zhong · Aerospace Science and Technology · 2019 · 37 citations

Engineering, Computational Engineering, Mechanical Engineering +15

Effects of vortex dynamics mechanism of blade-end treatment on the flow losses in a compressor cascade at critical condition

Xiaoxu Kan, Wanyang Wu, Jingjun Zhong · Aerospace Science and Technology · 2020 · 37 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Research Progress of Tip Winglet Technology in Compressor

Jingjun Zhong, Wanyang Wu, Shaobing Han · Journal of Thermal Science · 2020 · 36 citations

Engineering, Aerospace Engineering, Mechanical Engineering +13