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Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
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Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
Dual channels of helicity cascade in turbulent flows 期刊论文
JOURNAL OF FLUID MECHANICS, 2020, 卷号: 894, 页码: 13
Authors:  Yan Z(闫政);  Li XL(李新亮);  Yu ZP(于长平);  Wang JC;  Chen SY
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homogeneous turbulence  isotropic turbulence  turbulence theory  
高速受电弓下框架等效阻尼的实验研究 期刊论文
实验力学, 2020, 卷号: 35, 期号: 03, 页码: 425-431
Authors:  张志奇;  吴孟臻;  燕永钊;  张颢辰;  吴荣平;  魏征;  许向红
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阻尼器  下臂下铰摩擦  气囊  下框架等效阻尼  解耦测量分析  
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
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Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction  
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition 期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
Authors:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟)
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Coupled flow-thermal analysis  Thermal protection system  Basic direct correction method (BDCM)  Improved DCM (IDCM)  Iteration solution method (ISM)  
Scale locality of helicity cascade in physical space 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 6, 页码: 6
Authors:  Yan Z(闫政);  Li XL(李新亮);  Yu ZP(于长平)
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一种高硬度高电导率梯度结构Cu-Cr 合金触头的制备方法 专利
发明专利. 一种高硬度高电导率梯度结构Cu-Cr 合金触头的制备方法, 专利号: ZL201811267429.1, 申请日期: 2018-10-29, 授权日期: 2020-04-24
Inventors:  虞钢;  张犁天;  郑彩云;  何秀丽;  李少霞;  宁伟健
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边坡稳定分析的虚功率法 期刊论文
力学学报, 2020, 卷号: 52, 期号: 03, 页码: 663-672
Authors:  吴梦喜;  杨家修;  湛正刚
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边坡稳定  虚功率法  有限元  上限定理  
Aeroelastic Simulation Using CFD/CSD Coupling Based on Precise Integration Method 期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 页码: 18
Authors:  Huang CD(黄程德);  Huang J(黄杰);  Song X(宋鑫);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
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Flutter  Static aeroelasticity  CFD  CSD coupling  Precise integration method  
一种热疲劳实验方法 专利
发明专利. 一种热疲劳实验方法, 专利号: ZL201611101553.1, 申请日期: 2016-12-05, 授权日期: 2020-01-17
Inventors:  虞钢;  潘斯宁;  郑彩云;  何秀丽;  李少霞;  宁伟健
View  |  Adobe PDF(1808Kb)  |  Favorite  |  View/Download:8/1  |  Submit date:2020/08/13