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Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Favorite  |  View/Download：18/0  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
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
Authors:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
View  |  Adobe PDF(2082Kb)  |  Favorite  |  View/Download：33/1  |  Submit date：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
Deformation behavior of non-rigid airships in wind tunnel tests 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 3, 页码: 611-618
Authors:  Lu LL(路玲玲);  Song HW(宋宏伟);  Wang YW(王一伟);  Huang CG(黄晨光)
View  |  Adobe PDF(3480Kb)  |  Favorite  |  View/Download：114/6  |  Submit date：2019/01/09
Angle of attack  Fiber Bragg grating sensor  Flow velocity  Internal pressure  Non-rigid airship  Wind tunnel test  
Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1161Kb)  |  Favorite  |  View/Download：118/28  |  Submit date：2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
High-speed unsteady flows past two-body configurations 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 1, 页码: 54-64
Authors:  Xue XP;  Nishiyama Y;  Nakamura Y;  Mori K;  Wang YP(汪运鹏);  Wen CY
View  |  Adobe PDF(2278Kb)  |  Favorite  |  View/Download：45/12  |  Submit date：2018/10/30
Compressible flow  Shock/shock interaction  Two-body configurations  Unsteady flow  Wake/shock interaction  
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
Authors:  Huang CD(黄程德);  Liu W(刘文);  Yang GW(杨国伟)
View  |  Adobe PDF(4021Kb)  |  Favorite  |  View/Download：160/44  |  Submit date：2017/11/29
Aeroelasticity  Fluid-structure Interpolation  Grid Fin  Mesh Deformation  Radial Basis Function  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1080Kb)  |  Favorite  |  View/Download：292/59  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
A novel intelligent adaptive control of laser-based ground thermal test 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 4, 页码: 1018-1026
Authors:  Gan ZT;  Yu G(虞刚);  Li SX(李少霞);  He XL(何秀丽);  Chen R;  Zheng CY(郑彩云);  Ning WJ(宁伟健);  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Adv Mfg, Beijing 100190, Peoples R China.
View  |  Adobe PDF(926Kb)  |  Favorite  |  View/Download：101/27  |  Submit date：2016/12/08
Adaptive Control  Fuzzy Logic  Ground Thermal Test  Laser Heating  Thermal Control  
A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 6, 页码: 1517-1526
Authors:  Chen S;  Sun QH(孙泉华)
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Radical recombination in a hydrocarbon-fueled scramjet nozzle 期刊论文
Chinese Journal of Aeronautics, 2014, 卷号: 27, 期号: 6, 页码: 1413-1420
Authors:  Zhang XY(张晓源);  Qin LZ;  Chen H(陈宏);  He XZ;  Liu Y;  Qin, LZ (reprint author), Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China.
View  |  Adobe PDF(1799Kb)  |  Favorite  |  View/Download：321/60  |  Submit date：2015/03/11
Chemical Reactions  Nozzles  Performance Calculation  Radical  Recombination