Selected(0)Clear
Items/Page: Sort: |
| 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:343/107  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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:273/84  |  Submit date:2020/08/26 Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |
| 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:437/102  |  Submit date:2019/05/29 Heat transfer measurement Lateral heat conduction Shock tunnel Thermocouple Hypersonic |
| Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 Authors: Wang Q(汪球); Lu P(卢盼); Li JW(栗继伟); Wu S(吴松); Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林) Adobe PDF(299Kb)  |  Favorite  |  View/Download:107/38  |  Submit date:2023/03/17 |
| Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel 期刊论文 JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381 Authors: Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林) View  |  Adobe PDF(1208Kb)  |  Favorite  |  View/Download:689/139  |  Submit date:2018/10/30 copper calorimeter high enthalpy shock tunnel heat transfer hypersonic |
| Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林) View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download:411/77  |  Submit date:2018/01/16 Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
| Performance of a detonation driven shock tunnel 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX View  |  Adobe PDF(468Kb)  |  Favorite  |  View/Download:316/85  |  Submit date:2018/01/16 Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |