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Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16
作者:  Chang SY(常思源);  Xiao Y(肖尧);  Li GL(李广利);  Tian ZW(田中伟);  Cui K(崔凯)
收藏  |  浏览/下载：70/0  |  提交时间：2024/01/22
High-pressure capturing wing  Subsonic  Numerical simulation  Wing dihedral  Stability  
Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15
作者:  Chang SY(常思源);  Xiao Y(肖尧);  Li GL(李广利);  Tian ZW(田中伟);  Cui K(崔凯)
Adobe PDF(8136Kb)  |  收藏  |  浏览/下载：43/3  |  提交时间：2024/03/11
High-pressure capturing wing  Hypersonic  Numerical simulation  Wing dihedral  Stability  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载：270/107  |  提交时间：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
作者:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
Adobe PDF(2859Kb)  |  收藏  |  浏览/下载：254/98  |  提交时间：2021/02/09
Aerodynamic thermal  Opposing jets  Parametric sensitivity analysis  Uncertainty quantification  Analysis of Variance  Non-Intrusive Polynomial Chaos  
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
作者:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3818Kb)  |  收藏  |  浏览/下载：411/103  |  提交时间：2020/11/30
Optimization design  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
作者:  Chen XJ;  Qiu ZP;  Wang XJ;  Li YL;  Wang RX(王睿星)
浏览  |  Adobe PDF(4860Kb)  |  收藏  |  浏览/下载：390/87  |  提交时间：2018/02/08
Uncertain Reduced-order Modeling  Robust Flutter Analysis  Interval Perturbation Method  Uncertain Aeroelastic System  
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
作者:  Li HX(李慧鑫);  Ye L(叶亮);  Wei XL(魏小林);  Li T(李腾);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1708Kb)  |  收藏  |  浏览/下载：457/199  |  提交时间：2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance