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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