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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
Authors: Jiang YZ; Wen CY; Zhang DL(张德良)
 Adobe PDF(6207Kb) |  Favorite | View/Download：264/102 | Submit date：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
Authors: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | Favorite | View/Download：285/113 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Three-dimensional simulation of ligament formation and breakup caused by external vibration 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 8, 页码: 17
Authors: Li YK; Zhang M; Wu K(吴坤)
Adobe PDF(14652Kb) | Favorite | View/Download：401/97 | Submit date：2020/10/23 |
| Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8
Authors: Du MM(杜蒙蒙); Zhong FQ(仲峰泉); Xing YF(邢云绯); Zhang XY(张新宇)
Adobe PDF(2316Kb) | Favorite | View/Download：287/115 | Submit date：2020/08/26
Impingement jets Kerosene Heat transfer coefficient Pressure loss Reynolds number |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒)
Adobe PDF(1090Kb) | Favorite | View/Download：276/101 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Flow Modulation and Mixing Enhancement of Highly Underexpanded Jet by Vortex Excitation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2462-2474
Authors: Wang Y(汪也); Wu K(吴坤); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(6305Kb) | Favorite | View/Download：364/94 | Submit date：2020/07/06 |
| 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)
Adobe PDF(4182Kb) | Favorite | View/Download：303/88 | Submit date：2020/06/22
Coupled flow-thermal analysis Thermal protection system Basic direct correction method (BDCM) Improved DCM (IDCM) Iteration solution method (ISM) |
| 可压缩转捩及湍流的大涡模拟模型与应用 学位论文
博士论文，北京: 中国科学院大学, 2020
Authors: 周浩
Adobe PDF(11560Kb) | Favorite | View/Download：531/19 | Submit date：2020/06/08
可压缩流动 转捩及湍流 大涡模拟 建模 |
| Design and Optimization Method for Hypersonic Quasi-Waverider 期刊论文
AIAA Journal, 2020, 卷号: 58, 期号: 5, 页码: 2132-2146
Authors: Liu W(刘文); Zhang CA(张陈安); Wang FM(王发民); Ye ZY
Adobe PDF(1916Kb) | Favorite | View/Download：559/133 | Submit date：2020/05/07 |
| Development of a stagnation streamline model for thermochemical nonequilibrium flow 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 4, 页码: 046102
Authors: Hong QZ(洪启臻); Wang XY(王小永); Hu Y(胡远); Sun QH(孙泉华)
 View |  Adobe PDF(2694Kb) | Favorite | View/Download：453/126 | Submit date：2020/04/21
Hypersonic |
