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Effect of the trailing-edge flap on tones due to self-excited oscillation within the leading-edge slat cove 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 卷号: 237, 期号: 4, 页码: 853-864./通讯作者：Guo, H (corresponding author), Beihang Univ, Inst Fluid Mech, Beijing 100191, Peoples R China.
Authors:  Lu WS(陆维爽);  Liu, Peiqing;  Guo, Hao
Adobe PDF(3537Kb)  |  Favorite  |  View/Download：268/56  |  Submit date：2022/10/23
high-lift device  leading-edge slat  aerodynamic noise  acoustic characteristics  trailing-edge flap  
Numerical study on aerodynamic performance of waverider with a new bluntness method 期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233./通讯作者：Li, G.
Authors:  Qu ZP;  Xiao HD;  Lv MY;  Li GL(李广利);  Cui K(崔凯)
Adobe PDF(1179Kb)  |  Favorite  |  View/Download：315/128  |  Submit date：2021/06/11
bluntness method  computational fluid dynamics  hypersonic  volume  Waverider  
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
Authors:  Xiao YB(肖雅斌);  Yue LJ(岳连捷);  Ma SH;  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
View  |  Adobe PDF(1353Kb)  |  Favorite  |  View/Download：541/127  |  Submit date：2016/09/14
Hypersonic Inlet  Shape Transition  Inward Turning  Scramjet  Design Method