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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:  Yang L;  岳连捷;  张启帆;  张新宇
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Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
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Spacecraft  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
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Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
Adobe PDF(1674Kb)  |  Favorite  |  View/Download：451/118  |  Submit date：2014/02/24