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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:53/25  |  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:83/33  |  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:386/68  |  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:295/82  |  提交时间:2018/01/16 Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |