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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:154/39  |  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 |
| 机体尾缘形状对高压捕获翼构型亚声速特性影响 期刊论文 航空学报, 2022, 期号: 06, 页码: 16 作者: 王浩祥; 肖尧; 张凯凯; 李广利; 常思源; 田中伟; 崔凯 Adobe PDF(2111Kb)  |  收藏  |  浏览/下载:166/46  |  提交时间:2022/10/17 高压捕获翼 亚声速 流动特性 流动分离 数值模拟 |
| Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 14 作者: Zhou, Lin; Teng, Honghui; Ng, Hoi Dick; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(6382Kb)  |  收藏  |  浏览/下载:225/34  |  提交时间:2021/11/01 Cellular detonation Lead shock evolution Multi-layer perceptron Numerical simulations |
| 激波/湍流边界层干扰压力脉动特性数值研究 期刊论文 力学学报, 2021, 卷号: 53, 期号: 07, 页码: 1829-1841 作者: 童福林; 段俊亦; 周桂宇; 李新亮 Adobe PDF(2418Kb)  |  收藏  |  浏览/下载:267/69  |  提交时间:2021/08/25 激波/湍流边界层干扰 压力脉动 功率谱密度 两点相关 时空关联 |
| Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363 作者: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮) Adobe PDF(4402Kb)  |  收藏  |  浏览/下载:204/47  |  提交时间:2021/06/07 Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| 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:284/57  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:202/50  |  提交时间:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 作者: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:260/101  |  提交时间:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows 期刊论文 ACTA MECHANICA SINICA, 2020, 页码: 9 作者: Qi H(齐涵); Li XL(李新亮); Yu ZP(于长平) Adobe PDF(2084Kb)  |  收藏  |  浏览/下载:352/81  |  提交时间:2020/07/06 Large-eddy simulation Subgrid-scale model Rotating turbulent channel flow |
| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177 作者: Yao W(姚卫) 浏览  |  Adobe PDF(9586Kb)  |  收藏  |  浏览/下载:652/294  |  提交时间:2019/12/17 Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |