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| Magnetohydrodynamic experiments conducted in a detonation driven high enthalpy shock tunnel 会议论文
The 34thInternational Symposium on Shock Waves (ISSW34), Daegu, KOREA, July 16-21, 2023
Authors: Luo K(罗凯) ; Wang Q(汪球); Li JP(李进平); Zhao W(赵伟)
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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
Authors: 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) | Favorite | View/Download：267/51 | Submit date：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
Authors: 尚甲豪; 邢好运; 汪球; 李进平; 赵伟; 魏炳忱
Adobe PDF(3263Kb) | Favorite | View/Download：311/67 | Submit date：2022/06/10
爆轰驱动 轻气炮 数值模拟 发射性能 内弹道 |
| 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
Authors: 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) | Favorite | View/Download：576/109 | Submit date：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 |
| 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
Authors: 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)
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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
Authors: 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) | Favorite | View/Download：262/50 | Submit date：2021/11/01 |
| 基于高温气体效应的磁流体流动控制研究进展 期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1515-1531
Authors: 罗凯; 汪球; 李逸翔; 李进平; 赵伟
Adobe PDF(12949Kb) | Favorite | View/Download：298/72 | Submit date：2021/11/12
高超声速 高温真实气体效应 磁流体动力学 流动控制 气动力/热 |
| 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
Authors: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
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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
Authors: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏)
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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
Authors: 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) | Favorite | View/Download：278/101 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
