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超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  孟宇
Adobe PDF(11443Kb)  |  Favorite  |  View/Download:26/1  |  Submit date:2019/11/07
超燃冲压发动机,燃烧模态,火焰结构,加速过程,微波,滑移电弧,等离子体  
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:38/0  |  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:16/3  |  Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors:  Luo ZT(罗长童);  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Li JP(李进平);  Jiang ZL(姜宗林)
Favorite  |  View/Download:3/0  |  Submit date:2019/10/21
Aerodynamic force measurement  Dynamic system  Impact response  Cross-validation  System identification  
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:11/0  |  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:61/0  |  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:91/3  |  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:65/0  |  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:58/3  |  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:8/0  |  Submit date:2019/09/09
Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow