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| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40 作者: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(4374Kb)  |  收藏  |  浏览/下载:391/137  |  提交时间:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11 作者: Cheng D(程迪); Wang J(王晶); Lu Y(陆阳); Li L(李龙); Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(2651Kb)  |  收藏  |  浏览/下载:405/132  |  提交时间:2019/09/09 Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| Hypergolic ignition modulated by head-on collision, intermixing and convective cooling of binary droplets with varying sizes 期刊论文 INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 139, 页码: 475-481 作者: Zhang DW; Yu DH; Zhang P; Yuan YM(袁越明); Yue LJ(岳连捷); Zhang TC(张泰昌); Fan XJ(范学军) 浏览  |  Adobe PDF(1528Kb)  |  收藏  |  浏览/下载:313/114  |  提交时间:2019/09/09 |
| 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 作者: Wang Q(汪球); Olivier H; Einhoff J; Li JP(李进平); Zhao W(赵伟) 浏览  |  Adobe PDF(1085Kb)  |  收藏  |  浏览/下载:415/100  |  提交时间:2019/05/29 Heat transfer measurement Lateral heat conduction Shock tunnel Thermocouple Hypersonic |
| 高超声速飞行器红外窗口主动冷却技术研究 学位论文 硕士论文,北京: 中国科学院大学, 2019 作者: 舒开才 Adobe PDF(3193Kb)  |  收藏  |  浏览/下载:416/8  |  提交时间:2019/05/30 高超声速飞行器,红外窗口,主动冷却,蓝宝石 |
| 甲烷/氧气同轴射流层流高压燃烧扩散火焰稳定特性研究 学位论文 博士论文,北京: 中国科学院大学, 2019 作者: 葛逸飞 Adobe PDF(7841Kb)  |  收藏  |  浏览/下载:535/17  |  提交时间:2019/05/29 甲烷/氧气 同轴射流扩散火焰 层流火焰 燃烧不稳定 |
| Catalytic Recombination Characteristics of Atomic Oxygen on Material Surface by Optical Emission Spectroscopy 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 作者: Lin X(林鑫); Wang S(王苏); Li F(李飞); Zhang SH(张少华); Yu XL(余西龙) Adobe PDF(240Kb)  |  收藏  |  浏览/下载:25/9  |  提交时间:2023/03/17 |
| 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:54/25  |  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 |
| Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文 ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198 作者: Zhong K; Yan C; Chen SS; Wang XY(王小永); Ju SJ 浏览  |  Adobe PDF(8635Kb)  |  收藏  |  浏览/下载:213/71  |  提交时间:2019/05/29 Aeroheating Heatshield configuration Sphere-cone angle Mars Turbulent |