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| Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文 AIAA JOURNAL, 2024, 页码: 8 Authors: Wang WT(王文韬); Wang Q(汪球); Li JP(李进平); Zhao W(赵伟); Gao, Liangjie; Liu, Zhongchen; Qian, Zhansen Favorite  |  View/Download:80/0  |  Submit date:2024/02/26 Finite Element Method Hypersonic Shock Tube/Tunnel Diaphragm Burst Pressure |
| A quasi one dimensional model for the stagnation streamline in hypersonic magnetohydrodynamic flows 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 3, 页码: 36101 Authors: Luo K(罗凯); Wang Q(汪球); Li JP(李进平); Zhao W(赵伟); Gu, Sangdi Adobe PDF(4100Kb)  |  Favorite  |  View/Download:97/13  |  Submit date:2023/04/20 |
| 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) Favorite  |  View/Download:0/0  |  Submit date:2024/06/04 |
| Numerical and Experimental Study on the Duration of Nozzle Starting of the Reflected High-Enthalpy Shock Tunnel 期刊论文 APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 6, 页码: 16 Authors: Yu JP(于江鹏); Li JP(李进平); Wang Q(汪球); Zhang XY(张晓源); Zhang SZ(张仕忠) Adobe PDF(6583Kb)  |  Favorite  |  View/Download:364/156  |  Submit date:2022/05/17 nozzle starting high-enthalpy shock tunnel center startup complete startup |
| Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文 SHOCK WAVES, 2021, 页码: 8 Authors: 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)  |  Favorite  |  View/Download:289/66  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:360/111  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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 Authors: 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)  |  Favorite  |  View/Download:309/67  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:278/85  |  Submit date:2020/08/26 Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |
| Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文 EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478 Authors: Luo ZT(罗长童); Wang YP(汪运鹏); Hu ZM(胡宗民); Li JP(李进平); Jiang ZL(姜宗林) View  |  Adobe PDF(2227Kb)  |  Favorite  |  View/Download:293/69  |  Submit date:2019/10/21 Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文 EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66 Authors: Wang Q(汪球); Olivier H; Einhoff J; Li JP(李进平); Zhao W(赵伟) View  |  Adobe PDF(1085Kb)  |  Favorite  |  View/Download:446/104  |  Submit date:2019/05/29 Heat transfer measurement Lateral heat conduction Shock tunnel Thermocouple Hypersonic |