Liu Jun,袁化成,Yuan Hua Cheng,张锦昇,匡正.A Multifidelity Simulation Method for Internal and External Flow of a Hypersonic Airbreathing Pro....[J]:Aerospace,2022,9(685)

Jun Liu,Huacheng Yuan,Jingzhe Chen.Reynolds number effect on aerodynamic and starting charac-teristics of a two dimensional hyperson....[J]:Aerospace,2022,9(811)

刘君,,Yuan Hua Cheng,陈文芳,郭荣伟.Investigation of translation scheme turbine-based combined-cycle inlet mode transition.[J].France:Aerospace Science and Technology,2021,116(2021):106894

Yuan Hua Cheng,Yuan Hua Cheng,Liu Jun,guorongwei.一种Ma0～4 TBCC进气道气动设计及性能分析:实验流体力学,2018

Yuan Hua Cheng,Yuan Hua Cheng,Liu Jun,姚猛,gn.Numerical Simulation of Terminal Shock Oscillation in Over/Under Turbine-Based Combined-Cycle Inl...:INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,2017

Yuan Hua Cheng,Yuan Hua Cheng,Liu Jun,王云飞,gn.Unsteady supercritical/critical dual flowpath inlet flow and its control methods:CHINESE JOURNAL OF AERONAUTICS,2017

Yuan Hua Cheng,Yuan Hua Cheng,Liu Jun,gn.The flowfield and performance analyses of turbine-based combined cycle inlet mode transition at c...:AEROSPACE SCIENCE AND TECHNOLOGY,2017

Yuan Hua Cheng,Yuan Hua Cheng,陈文芳,Liu Jun,华正旭.基于圆锥截线的高超前体气动设计及特性分析:推进技术,2017

Yuan Hua Cheng,Yuan Hua Cheng,Liu Jun,华正旭,陈文芳,gn.Preliminary research of terminal shock motion in tandem configuration turbine-based combined cycl...:Aeronautical Journal,2017

Yuan Hua Cheng,Yuan Hua Cheng,Liu Jun,gn.Turbine based combined cycle inlet mode transition at different operation conditions:Int. Space Planes Hypersonics Technol. Conf.,2017