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Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载：268/107  |  提交时间：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
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  
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  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
作者:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1657Kb)  |  收藏  |  浏览/下载：266/91  |  提交时间：2020/08/26
Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22
作者:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
Adobe PDF(7457Kb)  |  收藏  |  浏览/下载：241/87  |  提交时间：2020/07/06
Aeroacoustics  Rod-airfoil configuration  Cell-centered finite difference method  Delayed detached eddy simulation  FW-H acoustic analogy  
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
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
浏览  |  Adobe PDF(3918Kb)  |  收藏  |  浏览/下载：521/165  |  提交时间：2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
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