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| 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:243/43  |  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 |
| 气相爆轰驱动二级轻气炮内弹道数值模拟 期刊论文 力学学报, 2022, 卷号: 54, 期号: 03, 页码: 810-821 作者: 尚甲豪; 邢好运; 汪球; 李进平; 赵伟; 魏炳忱 Adobe PDF(3263Kb)  |  收藏  |  浏览/下载:269/57  |  提交时间:2022/06/10 爆轰驱动 轻气炮 数值模拟 发射性能 内弹道 |
| 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:337/49  |  提交时间:2021/09/07 High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
| Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics 期刊论文 PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11 作者: Yu JP(于江鹏); Li JP(李进平); Wang Q(汪球); Zhang SZ(张仕忠); Zhang XY(张晓源) Adobe PDF(3271Kb)  |  收藏  |  浏览/下载:247/48  |  提交时间:2021/11/01 |
| Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文 SHOCK WAVES, 2021, 页码: 8 作者: Wang Q(汪球); Li JP(李进平); Luo K(罗凯); Li JW(栗继伟); Zhao W(赵伟) Adobe PDF(1158Kb)  |  收藏  |  浏览/下载:256/57  |  提交时间:2021/05/17 Hypersonic Aerodynamic heating Detached bow shock Shock tube expansion tube |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8 作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟) Adobe PDF(2023Kb)  |  收藏  |  浏览/下载:323/103  |  提交时间:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文 APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22 作者: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏) Adobe PDF(8566Kb)  |  收藏  |  浏览/下载:189/45  |  提交时间:2020/11/30 calorimeter shock tunnel heat transfer measurement hypersonic |
| 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 |
| Performance and Modeling of a Two-Stage Light Gas Gun Driven by Gaseous Detonation 期刊论文 APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 12, 页码: 16 作者: Tang WQ(唐伟奇); Wang Q(汪球); Wei BC(魏炳忱); Li JW(栗继伟); Li JP(李进平); Shang JH(尚甲豪); Zhang K(张坤); Zhao W(赵伟) Adobe PDF(6798Kb)  |  收藏  |  浏览/下载:302/65  |  提交时间:2020/08/26 two-stage light gas gun detonation quasi-one-dimensional piston projectile |
| Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475 作者: Wang Q(汪球); Luo K(罗凯); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟) Adobe PDF(2057Kb)  |  收藏  |  浏览/下载:261/82  |  提交时间:2020/08/26 Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |