Liu Jun
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Gender:Male
Education Level:With Certificate of Graduation for Doctorate Study
Alma Mater:南京航空航天大学
Scientific Research
Current position:
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Scientific Research
Research Field
Turbine-based combined cycle inlet and mode transition
Airframe/propulsion system integrated simulation method
Paper Publications
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Liu Jun. A Multifidelity Simulation Method for Internal and External Flow of a Hypersonic Airbreathing Propulsion System.Aerospace.2022,9(685)
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Jun Liu. Reynolds number effect on aerodynamic and starting charac-teristics of a two dimensional hypersonic inlet.Aerospace.2022,9(811)
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刘君. Investigation of translation scheme turbine-based combined-cycle inlet mode transition.Aerospace Science and Technology.2021,116(2021):106894
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Yuan Hua Cheng. 一种Ma0～4 TBCC进气道气动设计及性能分析.实验流体力学.2018
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Yuan Hua Cheng. Numerical Simulation of Terminal Shock Oscillation in Over/Under Turbine-Based Combined-Cycle Inlet.INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES.2017