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| Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 卷号: 44, 期号: 41, 页码: 23429-23435 作者: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民) 浏览  |  Adobe PDF(1085Kb)  |  收藏  |  浏览/下载:262/83  |  提交时间:2019/10/21 Oblique detonation wave Boundary layer Viscosity Detonation initiation Hydrogen-air mixture |
| 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) Adobe PDF(3918Kb)  |  收藏  |  浏览/下载:526/167  |  提交时间:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文 AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523 作者: Chen H; Tan H; Liu YZ; Zhang QF(张启帆) Adobe PDF(4679Kb)  |  收藏  |  浏览/下载:272/97  |  提交时间:2019/09/09 |
| 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) Adobe PDF(2165Kb)  |  收藏  |  浏览/下载:403/93  |  提交时间:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| 真实气体效应对Ma10级进气道流动的影响 期刊论文 推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050 作者: 张启帆; 岳连捷; 贾轶楠; 张新宇; 李欣; 高雄 Adobe PDF(1675Kb)  |  收藏  |  浏览/下载:210/44  |  提交时间:2019/09/12 真实气体效应 高马赫数进气道 化学非平衡气体模型 热完全气体模型 前缘钝化 再起动性能 |
| Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(714Kb)  |  收藏  |  浏览/下载:31/15  |  提交时间:2023/03/17 |