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| Influence of Dual Ignition on Test Conditions of a High-Enthalpy Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Wang Q(汪球); Zhao W(赵伟) ; Li JW(栗继伟); Li JP(李进平); Lu P(卢盼); Jiang ZL(姜宗林)
 Adobe PDF(240Kb) |  收藏 | 浏览/下载：51/25 | 提交时间：2023/03/17 |
| 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
作者: 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) | 收藏 | 浏览/下载：75/29 | 提交时间：2023/03/17 |
| 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
作者: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
 浏览 | Adobe PDF(679Kb) | 收藏 | 浏览/下载：380/66 | 提交时间：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
作者: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX
浏览 | Adobe PDF(468Kb) | 收藏 | 浏览/下载：290/81 | 提交时间：2018/01/16
Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |
