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Tests on the Accuracy and Scalability of the Full-Potential DFT Method Based on Multiple Scattering Theory 期刊论文
FRONTIERS IN CHEMISTRY, 2020, 卷号: 8, 页码: 590047
作者:  Cao PY(曹沛宇);  Fang J;  Gao XY;  Tian FY;  Song HF
Adobe PDF(1650Kb)  |  收藏  |  浏览/下载:212/33  |  提交时间:2021/02/09
first principles  Korringa-Kohn-Rostoker (KKR)  multiple scattering theory (MST)  full potential  elastic constants  
Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
作者:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
Adobe PDF(6207Kb)  |  收藏  |  浏览/下载:238/95  |  提交时间:2021/02/09
非平坦地形作用下自由表面波与界面波的理论与数值研究 学位论文
博士论文,北京: 中国科学院大学, 2020
作者:  王冕
Adobe PDF(7435Kb)  |  收藏  |  浏览/下载:194/10  |  提交时间:2021/06/10
重力波  变化非平坦地形  完全非线性Euler 方程  浅水方程组  
Design of a new supersonic biplane 期刊论文
Acta Astronautica, 2020, 卷号: 175, 期号: 10, 页码: 216-233
作者:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW
Adobe PDF(5403Kb)  |  收藏  |  浏览/下载:443/56  |  提交时间:2020/06/08
On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 41, 页码: 21940-21955
作者:  Yao W(姚卫)
Adobe PDF(3791Kb)  |  收藏  |  浏览/下载:258/131  |  提交时间:2020/09/27
Dynamic zone flamelet model  Supersonic hydrogen jet  Large eddy simulation  Supersonic combustion  Turbulent combustion model  
分形声学超材料结构设计与声学特性研究 学位论文
博士论文,北京: 中国科学院大学, 2020
作者:  刘宇
Adobe PDF(7396Kb)  |  收藏  |  浏览/下载:311/11  |  提交时间:2020/09/01
空间折叠  低频、宽频隔声  分形结构  双负特性  
Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22
作者:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
Adobe PDF(7457Kb)  |  收藏  |  浏览/下载:240/87  |  提交时间:2020/07/06
Aeroacoustics  Rod-airfoil configuration  Cell-centered finite difference method  Delayed detached eddy simulation  FW-H acoustic analogy  
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
作者:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3251Kb)  |  收藏  |  浏览/下载:337/111  |  提交时间:2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction  
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
作者:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  收藏  |  浏览/下载:315/84  |  提交时间:2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
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
作者:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟)
Adobe PDF(4182Kb)  |  收藏  |  浏览/下载:275/86  |  提交时间:2020/06/22
Coupled flow-thermal analysis  Thermal protection system  Basic direct correction method (BDCM)  Improved DCM (IDCM)  Iteration solution method (ISM)