Efficient Design Method for Applying Vortex Generators in Turbomachinery von Li, Jiabin, Ji, Lucheng

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Vortex generator evaluation models and flow mechanisms for compressor cascade von Ren, Xinyu, Meng, Tongtong, Zhu, Huiling, Ji, Lucheng

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Application of New Empirical Models based on Mathematical Statistics in the Through-Flow Analysis von Fei, Teng, Ji, Lucheng

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Leading edge redesign of dual-peak type variable inlet guide vane and its effect on aerodynamic performance von Shi, Hengtao, Ji, Lucheng

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Control and Entropy Analysis of Corner Flow Separation in a Compressor Cascade Using Streamwise Grooves von Yi, Weilin, Ji, Lucheng

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PIV investigation on corner separation control in a compressor cascade based on a vortex generator von Sun, Shuxian, Zhou, Ling, Zhu, Yichen, Zhu, Huiling, Meng, Tongtong, Ji, Lucheng

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Effect of inlet total pressure non-uniform distribution on aerodynamic performance and flow field of turbine von Wentong, Shi, Weilin, Yi, Lucheng, Ji

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Experimental investigation on the performance of compressor cascade using blended-blade-end-wall contouring technology von Yi, Weilin, Ji, Lucheng

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Study of Circumferential Grooved Casing Treatment on Cascade Aerodynamic Performance von Tan, Jingbo, Zhang, Chun, Zhu, Huiling, Zhou, Ling, Ji, Lucheng

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Study on aerodynamic optimal super/transonic turbine cascade and its geometry characteristics von Ji, Lucheng, Yu, Jia, Li, Weiwei, Yi, Weilin

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Full blended blade and endwall design of a compressor cascade von MENG, Tongtong, YANG, Guang, ZHOU, Ling, JI, Lucheng

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Influence of sub boundary layer vortex generator height and attack angle on cross-flows in the hub region of compressors von FU, Hao, ZHOU, Ling, JI, Lucheng

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Integrated passage design based on extended free-form deformation and adjoint optimization von LI, Xin, MENG, Tongtong, Li, Weiwei, ZHOU, Ling, JI, Lucheng

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Numerical investigation of the effects of rising angle on intermediate turbine duct and nearby turbines von Liu, Hongrui, Ji, Lucheng, Liu, Jun, Du, Qiang, Liu, Guang, Wang, Pei, Du, Meimei

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Aerodynamic adjoint optimization of turbomachinery with direct control on blade design parameters von LI, Xin, MENG, Tongtong, LI, Weiwei, ZHOU, Ling, JI, Lucheng

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Investigation of Hysteresis Loop in the Starting Process of Supersonic Cascade von Zhang, Shuying, Zhou, Ling, Ji, Lucheng

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Influence of Solidity on Aerodynamic Performance of Axial Supersonic Through-Flow Fan Cascades von Sun, Shijun, Zhou, Ling, Ji, Lucheng

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Experimental and numerical research on blended blade and end wall technique in a compressor cascade von Meng, Tongtong, Li, Xin, Zhou, Ling, Ji, Lucheng

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Corner stall control in linear compressor cascade by blended blade and endwall technique based on large eddy simulation von Zhu, Huiling, Zhou, Ling, Meng, Tongtong, Ji, Lucheng

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A Free Surface Sharpening Strategy Using Optimization Method von Song, Hongchao, Ji, Lucheng, Tu, Shuangzhang

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