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| 基于主动射流控制的高超声速进气道再起动性能研究(英文) 期刊论文 Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662 作者: 靳一超; 姚卫 Adobe PDF(1844Kb)  |  收藏  |  浏览/下载:137/35  |  提交时间:2023/02/09 高超声速进气道 不起动 再起动 主动射流 流动控制 |
| 斜爆轰推进中的起爆与驻定问题研究 学位论文 硕士论文,北京: 中国科学院大学, 2022 作者: 韩信 Adobe PDF(7629Kb)  |  收藏  |  浏览/下载:468/16  |  提交时间:2022/06/30 斜爆轰发动机 航空煤油RP-3 强制起爆 JF-12复现高超声速飞行条件激波风洞 斜爆轰波-边界层干扰 |
| Parameters for evaluating the efficiency of inlet compression 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56 作者: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(511Kb)  |  收藏  |  浏览/下载:195/37  |  提交时间:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文 AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882 作者: Huang TL(黄庭隆); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang P; Zhao QJ Adobe PDF(2961Kb)  |  收藏  |  浏览/下载:201/42  |  提交时间:2022/02/17 |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:278/54  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:376/61  |  提交时间:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文 COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436 作者: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(3599Kb)  |  收藏  |  浏览/下载:325/88  |  提交时间:2021/03/03 Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| 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:264/110  |  提交时间:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8 作者: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(1657Kb)  |  收藏  |  浏览/下载:265/91  |  提交时间:2020/08/26 Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| 矩形隔离段激波串非对称性及迟滞特性研究 学位论文 博士论文,北京: 中国科学院大学, 2020 作者: 黄庭隆 Adobe PDF(13697Kb)  |  收藏  |  浏览/下载:272/10  |  提交时间:2020/05/31 激波串 非对称 激波串迟滞 隔离段 斜楔 |