Hypersonic starting flow at high angle of attack von Bai, Chenyuan, Wu, Ziniu

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Generalized Kutta-Joukowski theorem for multi-vortex and multi-airfoil flow （a lumped vortex model） von Bai Chenyuan Wu Ziniu

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Generalized Kutta–Joukowski theorem for multi-vortex and multi-airfoil flow with vortex production——A general model von Bai, Chenyuan, Li, Juan, Wu, Ziniu

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A hypersonic lift mechanism with decoupled lift and drag surfaces von Xu, YiZhe, Xu, ZhiQi, Li, ShaoGuang, Li, Juan, Bai, ChenYuan, Wu, ZiNiu

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Symmetric Mach reflection configuration with asymmetric unsteady solution von BAI, Chenyuan, WANG, Miaomiao, WU, Ziniu

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Transit time difference and equal or non-equal transit time theory for airfoils with lift von BAI, Chenyuan, WU, Ziniu

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Generalized Kutta–Joukowski theorem for multi-vortex and multi-airfoil flow (a lumped vortex model) von Bai, Chenyuan, Wu, Ziniu

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Mach reflection in steady supersonic flow considering wedge boundary-layer correction von CHEN, Zijun, BAI, Chenyuan, WU, Ziniu

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Subsonic impulsively starting flow at a high angle of attack with shock wave and vortex interaction von BAI, Chenyuan, LI, Juan, WU, Ziniu

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A self-similar solution of a curved shock wave and its time-dependent force variation for a starting flat plate airfoil in supersonic flow von CHEN, Zijun, LIN, Jing, BAI, Chenyuan, WU, Ziniu

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Turbulent Wagner problem with transition von LI, Sicheng, BAI, Chenyuan, LIN, Jing, WU, Ziniu

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80 years education of aerospace science and technology in Tsinghua University von LU, Jie, GAO, Yongli, WANG, Xiaojing, BAI, Chenyuan, WANG, Bing, WU, Ziniu

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Review of theoretical achievements for starting flow problem for all Mach numbers von BAI, Chenyuan, LI, Juan, LI, Sheng, LI, Sicheng, WU, Ziniu

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