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Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
作者:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
浏览  |  Adobe PDF(2082Kb)  |  收藏  |  浏览/下载:417/189  |  提交时间:2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
Experimental investigation of liquid film cooling in hypersonic flow 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
作者:  Yuan CK(苑朝凯);  Li JP(李进平);  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
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The plasma morphology of an asymmetric electrode ablative pulsed plasma thruster 期刊论文
PLASMA SOURCES SCIENCE & TECHNOLOGY, 2019, 卷号: 28, 期号: 2, 页码: AR25008
作者:  Zhang Z;  Ling WYL;  Ren JX;  Tang HB;  Cao JB;  Lin X(林鑫);  York TM
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ablative pulsed plasma thruster  segmented anode  ultra-high-speed camera  arc morphology  
Life Science in Space: Experiments on Board the SJ-10 Recoverable Satellite 专著
Beijing;Singapore:Science Press; Springer, 2019
作者:  Editors: Duan EK;  Long M(龙勉)
Adobe PDF(21614Kb)  |  收藏  |  浏览/下载:261/0  |  提交时间:2019/12/18
Physical Science Under Microgravity: Experiments on Board the SJ-10 Recoverable Satellite 专著
Beijing;Singapore:Science Press; Springer, 2019
作者:  Hu WR(胡文瑞);  Kang Q(康琦);  Editors
Adobe PDF(20285Kb)  |  收藏  |  浏览/下载:254/0  |  提交时间:2019/12/18