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| Numerical study of wedge-induced oblique detonations in unsteady flow 期刊论文
JOURNAL OF FLUID MECHANICS, 2019, 卷号: 876, 页码: 264-287
Authors: Yang PF(杨鹏飞); Ng HD; Teng HH(滕宏辉)
  Favorite | View/Download：30/0 | Submit date：2019/09/09
detonations |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: 1-8
Authors: Gu HB(顾洪斌)
 View |  Adobe PDF(3099Kb) | Favorite | View/Download：7/0 | Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY张新宇
Favorite | View/Download：6/0 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Wall Temperature Effects on the Reynold Stress of Flat-Plate Turbulent Boundary Layer: a Numerical Investigation 期刊论文
ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2019, 卷号: 11, 期号: 3, 页码: 653-663
Authors: Li X(李欣); Yu ZP(于长平); Li XL(李新亮)
Favorite | View/Download：56/0 | Submit date：2019/04/11
Hypersonic direct numerical simulation wall temperature Reynold stress |
| Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors: Chen XP; Li XL(李新亮); Zhu ZC
View | Adobe PDF(4095Kb) | Favorite | View/Download：87/2 | Submit date：2019/04/11
direct numerical simulation velocity-temperature correlation supersonic flow channel flow thermally perfect gas strong Reynolds analogy |
| Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
Authors: Wang Q(汪球); Olivier H; Einhoff J; Li JP(李进平); Zhao W(赵伟)
Favorite | View/Download：59/0 | Submit date：2019/05/29
Heat transfer measurement Lateral heat conduction Shock tunnel Thermocouple Hypersonic |
| 高速飞行器发动机尾焰红外辐射目标特性计算方法 学位论文
博士论文，北京: 中国科学院大学, 2019
Authors: 丛彬彬
Adobe PDF(6916Kb) | Favorite | View/Download：54/2 | Submit date：2019/07/12
高速飞行器 高温尾焰 超声速射流 红外辐射 光线追踪 谱线筛选 |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
Favorite | View/Download：5/0 | Submit date：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| Fractal characterization of ceramic crack patterns after thermal shocks 期刊论文
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 2019, 卷号: 102, 期号: 6, 页码: 3641-3652
Authors: Qi F; Meng SH; Song F(宋凡); Guo H; Xu XH(许向红); Shao YF(邵颖峰); Chen Y
View | Adobe PDF(2401Kb) | Favorite | View/Download：51/10 | Submit date：2019/01/09
brittle materials crack growth fractal geometry thermal shock resistance |
| 高超声速飞行器红外窗口主动冷却技术研究 学位论文
硕士论文，北京: 中国科学院大学, 2019
Authors: 舒开才
Adobe PDF(3193Kb) | Favorite | View/Download：33/1 | Submit date：2019/05/30
高超声速飞行器，红外窗口，主动冷却，蓝宝石 |
