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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:270/107  |  提交时间:2021/11/01 Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| 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:255/103  |  提交时间:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163 作者: Wang XJ; Wang RX(王睿星); Wang L; Chen XJ; Geng XY 浏览  |  Adobe PDF(3200Kb)  |  收藏  |  浏览/下载:480/108  |  提交时间:2018/10/30 Non-probabilistic reliability based multidisciplinary design optimization Single loop strategy Uncertainty multidisciplinary analysis Non-probabilistic reliability analysis Translating distance calculation |
| Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230 作者: Chen XJ; Qiu ZP; Wang XJ; Li YL; Wang RX(王睿星) 浏览  |  Adobe PDF(4860Kb)  |  收藏  |  浏览/下载:390/87  |  提交时间:2018/02/08 Uncertain Reduced-order Modeling Robust Flutter Analysis Interval Perturbation Method Uncertain Aeroelastic System |