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Control of shock-wave/boundary-layer interaction using abackward-facing step 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13./通讯作者:Zhai, Jian
Authors:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW(张伟为)
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Shock-wave/boundary-layer interaction  Backward-facing step  Flow separation  Hypersonic inlet  
Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5./通讯作者:Zhang, Chen-An
Authors:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW
Adobe PDF(510Kb)  |  Favorite  |  View/Download:268/99  |  Submit date:2020/08/26
Hypersonic inlet  lateral spillage  waverider design method  streamline tracing technology  mass-flow ratio  
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:543/128  |  Submit date:2016/09/14
Hypersonic Inlet  Shape Transition  Inward Turning  Scramjet  Design Method  
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods 期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
View  |  Adobe PDF(1133Kb)  |  Favorite  |  View/Download:1170/275  |  Submit date:2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference  
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL(李广利);  Qu ZP(屈志朋);  Situ M;  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)