已选(0)清除
条数/页: 排序方式: |
| 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 |
| 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:262/58  |  提交时间:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| 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:377/61  |  提交时间:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247 作者: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(2818Kb)  |  收藏  |  浏览/下载:263/108  |  提交时间:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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 |
| 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:266/103  |  提交时间:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684 作者: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民); Deng, X 浏览  |  Adobe PDF(2321Kb)  |  收藏  |  浏览/下载:316/80  |  提交时间:2019/10/21 Oblique detonation wave Blunt wedge Initiation Hydrogen |
| 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 |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80 作者: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏) 浏览  |  Adobe PDF(2110Kb)  |  收藏  |  浏览/下载:368/135  |  提交时间:2018/10/30 Inlet restart Cowl shock Shock wave boundary layer interactions |
| 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:372/94  |  提交时间:2018/02/08 Oblique Detonation Equivalence Ratio Mixture Inhomogeneity Detailed Chemistry |