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| 高超声速喷管设计理论与方法 期刊论文 力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294 作者: 汪运鹏; 姜宗林 Adobe PDF(2086Kb)  |  收藏  |  浏览/下载:206/57  |  提交时间:2021/01/29 |
| 高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文 推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217 作者: 贺理浩; 张启帆; 岳连捷; 张新宇; 王卫星; 谭慧俊 Adobe PDF(9600Kb)  |  收藏  |  浏览/下载:236/34  |  提交时间:2021/11/12 高速进气道 低马赫数不起动 非定常 气动力 自起动 |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:320/168  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH(马生虎); Zhang QF(张启帆); Zhang, Peng; Zhang XY(张新宇) Adobe PDF(3937Kb)  |  收藏  |  浏览/下载:186/44  |  提交时间:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文 AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430 作者: Jiang YZ; Wen CY; Zhang DL(张德良) Adobe PDF(6207Kb)  |  收藏  |  浏览/下载:238/95  |  提交时间:2021/02/09 |
| 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:253/98  |  提交时间:2021/02/09 Aerodynamic thermal Opposing jets Parametric sensitivity analysis Uncertainty quantification Analysis of Variance Non-Intrusive Polynomial Chaos |
| Unsteady combustion mode with a super-high frequency induced by a curved shock 期刊论文 PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 11, 页码: 116101 作者: Teng HH(滕宏辉); Liu S; Zhang ZJ(张子健) Adobe PDF(5194Kb)  |  收藏  |  浏览/下载:253/69  |  提交时间:2020/12/28 PROJECTILE MECHANISM SYSTEMS |
| 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 |
| 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 |
| 廉价航天发射路在何方? 科普文章 2020 作者: 仝晓通 Adobe PDF(2158Kb)  |  收藏  |  浏览/下载:202/43  |  提交时间:2020/11/27 |