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| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:335/172  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| 传感器安装对平板气动热测量精度的影响 期刊论文 北京航空航天大学学报, 2020, 卷号: 47, 期号: 09, 页码: 1790-1798 作者: 罗凯; 汪球; 栗继伟; 李进平; 赵伟 Adobe PDF(2231Kb)  |  收藏  |  浏览/下载:209/57  |  提交时间:2021/11/12 平板 气动热 安装精度 雷诺数 边界层 |
| 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 |
| Coaxial Thermocouples for Heat Transfer Measurements in Long-Duration High Enthalpy Flows 期刊论文 SENSORS, 2020, 卷号: 20, 期号: 18, 页码: 18 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(7131Kb)  |  收藏  |  浏览/下载:293/89  |  提交时间:2020/11/30 heat transfer measurement coaxial thermocouple long-duration semi-infinite high enthalpy |
| 过热流动和闪急沸腾雾化过程的数值模拟研究 学位论文 博士论文,北京: 中国科学院大学, 2020 作者: 李亚超 Adobe PDF(22044Kb)  |  收藏  |  浏览/下载:492/7  |  提交时间:2020/08/27 过热流动,闪急沸腾雾化, 气泡生长模型,过热液滴破碎模型, 过热相变模型 |
| Wall-shear stress fluctuations in a supersonic turbulent boundary layer over an expansion corner 期刊论文 JOURNAL OF TURBULENCE, 2020, 页码: 20 作者: Tong FL(童福林); Chen JQ; Sun D; Li XL(李新亮) Adobe PDF(5228Kb)  |  收藏  |  浏览/下载:198/85  |  提交时间:2020/08/26 Wall-shear stress expansion corner supersonic turbulent boundary layer direct numerical simulation |
| 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 |
| 发动机冷却结构优化设计方法研究 学位论文 博士论文,北京: 中国科学院大学, 2020 作者: 李轩 Adobe PDF(8199Kb)  |  收藏  |  浏览/下载:326/11  |  提交时间:2020/06/01 火箭发动机,再生冷却,优化,变分 |