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| Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文 AIAA JOURNAL, 2022, 页码: 9 作者: Wu ZJ(吴振杰); Zhang QF(张启帆); Zhang X(张旭); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷) Adobe PDF(3049Kb)  |  收藏  |  浏览/下载:156/22  |  提交时间:2022/07/18 |
| 高马赫数燃烧强化的激波风洞试验研究 期刊论文 力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413 作者: 张旭; 张启帆; 岳连捷; 孟东东; 罗苇航; 于江鹏; 张晓源; 李进平; 陈宏; 李飞 Adobe PDF(3069Kb)  |  收藏  |  浏览/下载:234/43  |  提交时间:2022/08/11 高马赫数 超声速燃烧 燃烧强化 小支板 JF-24激波风洞 |
| 基于动态分区概念的高超声速燃烧大涡模拟 期刊论文 力学学报, 2022, 卷号: 54, 期号: 04, 页码: 954-974 作者: 姚卫; 刘杭; 张政; 肖雅彬; 岳连捷 Adobe PDF(1875Kb)  |  收藏  |  浏览/下载:266/62  |  提交时间:2022/06/10 高超声速燃烧 动态分区火焰面 分区自适应化学 分区并行自适应建表 改进延迟分离涡模拟 |
| 高马赫数超燃冲压发动机技术研究进展 期刊论文 力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288 作者: 岳连捷; 张旭; 张启帆; 陈科挺; 李进平; 陈昊; 姚卫; 仲峰泉; 李飞; 王春; 陈宏 Adobe PDF(2622Kb)  |  收藏  |  浏览/下载:522/97  |  提交时间:2022/03/16 高马赫数 超燃冲压发动机 热化学非平衡 超声速燃烧 低雷诺数流动 激波风洞 飞行试验 |
| Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文 AIAA JOURNAL, 2022, 页码: 7 作者: Zhang X(张旭); Zhang QF(张启帆); Wu ZJ(吴振杰); Yue LJ(岳连捷); Gao ZB(高占彪); Luo WH(罗苇航); Chen H(陈昊) Adobe PDF(1382Kb)  |  收藏  |  浏览/下载:152/27  |  提交时间:2022/03/22 |
| 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:201/39  |  提交时间:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| 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:265/58  |  提交时间:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815 作者: Zhou GX(周功喜); Zhang X(张旭); Li JP(李进平); Zhang XY(张晓源); Zhang SZ(张仕忠); Lin X(林鑫); Li F(李飞); Chen H(陈宏); Yue LJ(岳连捷); Yu XL(余西龙) Adobe PDF(4108Kb)  |  收藏  |  浏览/下载:331/48  |  提交时间:2021/09/07 High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
| Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788 作者: Xue, Rui; Zheng, Xing; Yue LJ(岳连捷); Zhang, Qian; He, Xin; Yang, Jing; Weng, Chao; Li, Zhihao Adobe PDF(5483Kb)  |  收藏  |  浏览/下载:126/42  |  提交时间:2022/10/25 Boundary layer combustion Skin-friction reduction Supersonic combustion Scramjet engine |
| 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:380/62  |  提交时间:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |