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高超声速气动弹性响应及热环境下的颤振特性研究 学位论文
博士论文,北京: 中国科学院大学, 2023
Authors:  黄杰
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高超声速飞行器  气动-热-结构耦合  壁板颤振  TPS壁板  直接积分法  
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Lai, Jiang;  Sun, Dong;  Yuan, Xianxu
Adobe PDF(4757Kb)  |  Favorite  |  View/Download:46/0  |  Submit date:2023/04/20
Shock wave  Hypersonic turbulent  boundary layer  Heat transfer  Skin friction decomposition  Direct numerical simulation  
Finite-wing-analogy formula for compressibility correction to pressure coefficient of an underwater vehicle model at low Mach number 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 1, 页码: 20
Authors:  Wang Y(王宇);  Liu Y(刘毅);  Zhou ZT(周志腾);  Wang SZ(王士召)
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GPU 加速的超大规模可压缩湍流直接数值模拟研究 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  党冠麟
Adobe PDF(39646Kb)  |  Favorite  |  View/Download:454/15  |  Submit date:2023/02/06
软件,湍流,高超声速,直接数值模拟,图形处理器  
再生冷却通道微结构强化传热与流动机理研究 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  李冼
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再生冷却  航空煤油  凹陷窝  微肋  强化传热  
Advances in Plasma Diagnostics and Applications 专著
Beijing:MDPI, 2022
Authors:  Editors:Chen ZT;  Attri P;  Wang Q(汪球)
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高超声速钝前缘乘波体优化设计研究 学位论文
硕士论文,北京: 中国科学院大学, 2022
Authors:  郭帅旗
Favorite  |  View/Download:170/10  |  Submit date:2022/07/08
高超声速  乘波体  前缘钝化  符号回归  
受电弓杆件气动噪声降噪研究 学位论文
硕士论文,北京: 中国科学院大学, 2022
Authors:  倪丹丹
Adobe PDF(5867Kb)  |  Favorite  |  View/Download:175/9  |  Submit date:2022/07/04
受电弓  气动噪声  大涡模拟  低噪声设计  
Aerodynamic-Aeroacoustic Optimization of a Baseline Wing and Flap Configuration 期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 3, 页码: 19
Authors:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Guo DL(郭迪龙);  Yang GW(杨国伟);  Wang YT(王业腾);  Yan C(闫畅)
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high-lift devices  computational fluid dynamics  computational aeroacoustics  Kriging surrogate model  optimization design  
A Direct-Forcing Immersed Boundary Method for Incompressible Flows Based on Physics-Informed Neural Network 期刊论文
Fluids, 2022, 卷号: 7, 期号: 2, 页码: 56
Authors:  Huang Y(黄毅);  Zhang ZY(张治愚);  Zhang X(张星)
Adobe PDF(6539Kb)  |  Favorite  |  View/Download:385/94  |  Submit date:2022/01/27
physics-informed neural networks (PINN)  direct-forcing immersed boundary method  incompressible laminar flow  circular cylinder