| Experimental and numerical investigation of smooth turbine-based combined-cycle inlet mode transition J Liu, H Yuan, Z Hua, W Chen, N Ge Aerospace Science and Technology 60, 124-130, 2017 | 29 | 2017 |
| Unsteady flow characteristic analysis of turbine based combined cycle (TBCC) inlet mode transition J Liu, H Yuan, G Rongwei Propulsion and Power Research 4 (3), 141-149, 2015 | 12 | 2015 |
| Unsteady supercritical/critical dual flowpath inlet flow and its control methods J. Liu, H. Yuan, Y. Wang, N. Ge Chinese Journal of Aeronautics 30 (6), 1877-1884, 2017 | 10 | 2017 |
| The flowfield and performance analyses of turbine-based combined cycle inlet mode transition at critical/subcritical conditions J Liu, H Yuan, N Ge Aerospace Science and Technology 69, 485-494, 2017 | 10 | 2017 |
| The design and validation of over/under turbine-based combined cycle inlet H Yuan, J Liu, J Zhang, Y Wang Aerospace Science and Technology 105, 105960, 2020 | 8 | 2020 |
| Analysis of over/under TBCC inlet mode transition flow characteristic J. Liu, H. Yuan, R. Guo Journal of Astronautics 37 (4), 461-469, 2016 | 8 | 2016 |
| Investigation of translation scheme turbine-based combined-cycle inlet mode transition J Liu, H Yuan, W Chen, R Guo Aerospace Science and Technology 116, 106894, 2021 | 7 | 2021 |
| Design and numerical simulation of a clamshell-shaped inlet cover for air-breathing hypersonic vehicles X Wen, J Liu, J Li, F Ding, Z Xia JOURNAL OF ZHEJIANG UNIVERSITY-SCIENCE A 20 (5), 347-357, 2019 | 6 | 2019 |
| Reynolds number effect on aerodynamic and starting characteristics of a two-dimensional hypersonic inlet J Liu, J Chen, H Yuan Aerospace 9 (12), 811, 2022 | 4 | 2022 |
| Evolution of turbulent boundary layer over a three-dimensional bump LIU Jun, D Fiscaletti, Y Huacheng Chinese Journal of Aeronautics 35 (6), 137-145, 2022 | 3 | 2022 |
| Numerical Simulation of Terminal Shock Oscillation in Over/Under Turbine-Based Combined-Cycle Inlet J Liu, H Yuan, M Yao, N Ge International Journal of Turbo & Jet-Engines, 2017 | 3* | 2017 |
| A multifidelity simulation method for internal and external flow of a hypersonic airbreathing propulsion system J Liu, H Yuan, J Zhang, Z Kuang Aerospace 9 (11), 685, 2022 | 2 | 2022 |
| Design and flow characteristics analysis of mode transition simulator for tandem type TBCC inlet J. Liu, H. Yuan, N. Ge Acta Aeronautica et Astronautica Sinica 2016 (12), 3675-3684, 2016 | 2* | 2016 |
| Design and validation of a two-dimensional variable geometry inlet H Yuan, Y Wang, J Liu, Z Hua International Journal of Turbo & Jet-Engines 40 (4), 473-480, 2023 | 1 | 2023 |
| Preliminary research of terminal shock motion in tandem configuration turbine-based combined cycle inlet J Liu, H Yuan, Z Hua, W Chen, N Ge The Aeronautical Journal 121 (1237), 416-432, 2017 | 1 | 2017 |
| Turbine Based Combined Cycle Inlet Mode Transition at Different Operation Conditions J Liu, H Yuan, N Ge 21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017 | 1 | 2017 |
| Integrated design and analysis of inlet and missile with two side layout F Liu, H Yuan, J Liu, L Xu, Z Zhou International Journal of Turbo & Jet-Engines 40 (s1), s539-s551, 2024 | | 2024 |
| Design and performance analysis of turbine based combined cycle inlet operation with Mach 0~ 4 Y Huacheng, L Jun, G Rongwei 实验流体力学 32 (3), 33-41, 2018 | | 2018 |
| Aerodynamic design and performance analysis of a two-dimensional variable geometry inlet H Yuan, Y Wang, J Liu, Z Hua 21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017 | | 2017 |
| Preliminary Research on Turbine-Based Combined-Cycle Inlet Flow Characteristics at Variable Inflow Conditions Y Huacheng, L Jun, G Rongwei Aerodynamic Research & Experiment 33 (4), 23, 0 | | |
