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Tan Huijun

Nanjing University of Aeronautics and Astronautics

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Publication

Featured researches published by Tan Huijun.

Science China-technological Sciences | 2007

A new concept and preliminary study of variable hypersonic inlet with fixed geometry based on shockwave control

Tan Huijun; Chen Zhi; Li Guangsheng

Archive | 2015

High-performance subsonic speed air inlet duct integrated with inner auxiliary air inlet duct

Tan Huijun; Sun Shu; Zhang Qifan; Du Mochen; Li Guangsheng

Archive | 2015

Embedded type air inlet channel using combined opening surface vortex control method

Tan Huijun; Sun Shu; Zhang Yue; Chen Hao; Li Guangsheng

Acta Aeronautica Et Astronautica Sinica | 2006

Characteristics of Shock Train in Two Dimensional Bends with Constant Area

Tan Huijun; Guo Rong-wei

Archive | 2014

Aircraft supersonic air inlet channel with variable deflation system

Tan Huijun; Sun Shu; Zhuang Yi; Wang Depeng; Li Guangsheng

Archive | 2015

Flow test system suitable for supersonic/hypersonic channel and test method

Tan Huijun; Huang Hexia; Cheng Lin; Yuan Yongqing; Sun Shu; Li Guangsheng

Archive | 2015

Universal design method for subsonic diffuser

Tan Huijun; Sun Shu; Huang Hexia; Bu Huanxian; Li Guangsheng

Journal of Aerospace Power | 2008

Effects of the forebody boundary layer state on flow structure and performance of hypersonic inlets

Tan Huijun

Archive | 2017

Control method of hydraulic servo driving system

Tan Huijun; Zhuang Yi; Zhang Yuchao; Wang Chenxi; Ling Yu; He Xiaoming

Archive | 2017

Secondary flow self-circulation pneumatic type adjustable air inflow passageway for in-step compression surface and control method

Tan Huijun; Wang Chenxi; Zhuang Yi; Sun Shu; Huang Hexia

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Collaboration

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Li Guangsheng

Nanjing University of Aeronautics and Astronautics

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Chen Zhi

Nanjing University of Aeronautics and Astronautics

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Guo Rong-wei

Nanjing University of Aeronautics and Astronautics

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