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Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
作者:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  收藏  |  浏览/下载：299/52  |  提交时间：2022/01/12
An sequential optimization and aeroelastic constraint transformation method for strength-aeroelastic comprehensive design 期刊论文
JOURNAL OF FLUIDS AND STRUCTURES, 2020, 卷号: 93, 页码: 14
作者:  Zhang ZS;  Wang XJ;  Chen XJ(陈贤佳)
浏览  |  Adobe PDF(2381Kb)  |  收藏  |  浏览/下载：274/87  |  提交时间：2020/04/07
Comprehensive design  Sequential optimization strategy  Airplane wing  Structural strength  Aeroelasticity  
Characterizing three-dimensional features of vortex surfaces in the flow past a finite plate 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 1, 页码: 15
作者:  Tong WW;  Yang Y(杨越);  Wang SZ(王士召)
Adobe PDF(6216Kb)  |  收藏  |  浏览/下载：248/93  |  提交时间：2020/05/18
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
作者:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
浏览  |  Adobe PDF(2082Kb)  |  收藏  |  浏览/下载：413/188  |  提交时间：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
High-Pressure Capturing Wing Configurations 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
作者:  Cui K(崔凯);  Li GL;  Xiao Y(肖尧);  Xu YZ;  Cui,K(reprint author), Chinese Acad Sci, Inst Mech
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载：616/170  |  提交时间：2017/07/24
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
浏览  |  Adobe PDF(1315Kb)  |  收藏  |  浏览/下载：335/128  |  提交时间：2017/11/29
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
作者:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
浏览  |  Adobe PDF(1133Kb)  |  收藏  |  浏览/下载：905/257  |  提交时间：2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference  
Interaction of isentropic compression waves with a bow shock 期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
作者:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(764Kb)  |  收藏  |  浏览/下载：744/278  |  提交时间：2014/01/17
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
作者:  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.
Adobe PDF(1426Kb)  |  收藏  |  浏览/下载：865/295  |  提交时间：2013/09/27
Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)  
Aerodynamic characteristics research on wide-speed range waverider configuration 期刊论文
Science in China Series E-Technological Sciences, 2009, 卷号: 52, 期号: 10, 页码: 2903-2910
作者:  Wang FM(王发民);  Ding HH(丁海河);  Lei MF(雷麦芳);  Wang FM
Adobe PDF(859Kb)  |  收藏  |  浏览/下载：652/210  |  提交时间：2009/08/03
Waverider Configuration  Aerodynamic Characteristics At Wide-speed Range  High Lift-to-drag Ratio