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| Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16 作者: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利); Tian ZW(田中伟); Cui K(崔凯) 收藏  |  浏览/下载:70/0  |  提交时间:2024/01/22 High-pressure capturing wing Subsonic Numerical simulation Wing dihedral Stability |
| 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 |
| 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 |
| Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8 作者: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙) Adobe PDF(1961Kb)  |  收藏  |  浏览/下载:267/103  |  提交时间:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781 作者: Zhong FQ(仲峰泉); Cheng LW(程柳维); Gu HB(顾洪斌); Zhang XY(张新宇) Adobe PDF(2032Kb)  |  收藏  |  浏览/下载:295/86  |  提交时间:2019/05/29 Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |