|
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：265/58 | 提交时间：2021/11/15
Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| 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：236/67 | 提交时间：2021/05/17
Oblique detonation Wave complex Instability Thermal choking Expansion corner |
| 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：254/98 | 提交时间：2021/02/09
Aerodynamic thermal Opposing jets Parametric sensitivity analysis Uncertainty quantification Analysis of Variance Non-Intrusive Polynomial Chaos |
| Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
作者: Ju SJ(鞠胜军); Sun ZX(孙振旭); Yang GW(杨国伟); Prapamonthon P; Zhang JY
Adobe PDF(3818Kb) | 收藏 | 浏览/下载：411/103 | 提交时间：2020/11/30
Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| 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：256/104 | 提交时间：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
作者: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇)
 Adobe PDF(3862Kb) | 收藏 | 浏览/下载：332/115 | 提交时间：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
作者: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林)
 浏览 | Adobe PDF(1937Kb) | 收藏 | 浏览/下载：262/86 | 提交时间：2018/10/30
Hypersonic Shock tunnel Start-up process Impulse force Vibration |
| Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者: Wang ZP(王知溥); Li F(李飞); Gu HS; Yu XL(余西龙); Zhang XY(张新宇); Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览 | Adobe PDF(1112Kb) | 收藏 | 浏览/下载：539/226 | 提交时间：2015/06/12
Scramjet Dual-mode Combustor Divergent Angle Cavity Location Combustion Efficiency Tdlas |
