|
已选(0)清除
条数/页： 排序方式： |
| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
作者: Yao W(姚卫) ; Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬)
 Adobe PDF(2954Kb) |  收藏 | 浏览/下载：261/57 | 提交时间：2021/11/15
Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
作者: Xue, Rui; Zheng, Xing; Yue LJ(岳连捷); Zhang, Qian; He, Xin; Yang, Jing; Weng, Chao; Li, Zhihao
Adobe PDF(5483Kb) | 收藏 | 浏览/下载：124/41 | 提交时间：2022/10/25
Boundary layer combustion Skin-friction reduction Supersonic combustion Scramjet engine |
| Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
作者: Wang KL(王宽亮); Yang PF(杨鹏飞); Teng HH(滕宏辉)
Adobe PDF(2853Kb) | 收藏 | 浏览/下载：233/67 | 提交时间：2021/05/17
Oblique detonation Wave complex Instability Thermal choking Expansion corner |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(8067Kb) | 收藏 | 浏览/下载：377/61 | 提交时间：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
作者: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(2818Kb) | 收藏 | 浏览/下载：263/108 | 提交时间：2021/01/29
Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
作者: Zhang W; Wang S; Wang Q; Ju SJ(鞠胜军); Yan C
Adobe PDF(2859Kb) | 收藏 | 浏览/下载：253/98 | 提交时间：2021/02/09
Aerodynamic thermal Opposing jets Parametric sensitivity analysis Uncertainty quantification Analysis of Variance Non-Intrusive Polynomial Chaos |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
作者: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | 收藏 | 浏览/下载：265/110 | 提交时间：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | 收藏 | 浏览/下载：306/98 | 提交时间：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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
作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
 浏览 | Adobe PDF(2165Kb) | 收藏 | 浏览/下载：394/92 | 提交时间：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏)
浏览 | Adobe PDF(2110Kb) | 收藏 | 浏览/下载：368/135 | 提交时间：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
