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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:273/60  |  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:239/67  |  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:387/65  |  提交时间:2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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:261/101  |  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:266/110  |  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:419/105  |  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:261/106  |  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)
浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载:337/117  |  提交时间:2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9
作者:  Fu YW(符耀威);  Yu ZP(于长平);  Yan Z(闫正);  Li XL(李新亮)
浏览  |  Adobe PDF(2894Kb)  |  收藏  |  浏览/下载:386/142  |  提交时间:2020/03/21
Supersonic combustion  Turbulence jet  Direct numerical simulations  Coherent structures  
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
作者:  Fang YS(方宜申);  Hu ZM(胡宗民);  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
浏览  |  Adobe PDF(2663Kb)  |  收藏  |  浏览/下载:377/94  |  提交时间:2018/02/08
Oblique Detonation  Equivalence Ratio  Mixture Inhomogeneity  Detailed Chemistry