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| 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：240/95 | 提交时间：2021/02/09 |
| Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
作者: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | 收藏 | 浏览/下载：254/103 | 提交时间：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 多脉冲毫秒激光打孔熔池动态演化机理研究 学位论文
博士论文，北京: 中国科学院大学, 2020
作者: 张越
 浏览 | Adobe PDF(11571Kb) | 收藏 | 浏览/下载：220/72 | 提交时间：2020/08/31
激光打孔 质量迁移 匙孔演化 熔池驱动力 时空传输特性 |
| A multi-time scale solution strategy for an elastomeric aircraft 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13
作者: Yang L(杨磊); Sun QH(孙泉华)
Adobe PDF(1858Kb) | 收藏 | 浏览/下载：214/89 | 提交时间：2020/08/26
Flight dynamic simulation Multi-time scale Elastomeric aircraft Reduced order models Store separation |
| 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：241/87 | 提交时间：2020/07/06
Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| An improved inverse method for multirow blades of turbomachinery 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2020, 页码: 11
作者: Li AT; Zhu YL; Li W; Wang X; Qin W(秦伟); Chen HS
Adobe PDF(1493Kb) | 收藏 | 浏览/下载：226/66 | 提交时间：2020/06/15
Inverse design method multirow blades turbomachinery load distribution transonic compressor |
| 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
作者: Huang CD(黄程德); Huang J(黄杰); Song X(宋鑫); Zheng GN(郑冠男); Nie XY(聂雪媛)
浏览 | Adobe PDF(5463Kb) | 收藏 | 浏览/下载：236/75 | 提交时间：2020/04/07
Flutter Static aeroelasticity CFD CSD coupling Precise integration method |
