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Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method 期刊论文
Aerospace Science and Technology, 2018, 卷号: 75, 页码: 200-214
作者:  Liu W(刘文);  Zhang CA(张陈安);  Wang FM(王发民)
浏览  |  Adobe PDF(2721Kb)  |  收藏  |  浏览/下载:533/116  |  提交时间:2018/06/16
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
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Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration  
An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163
作者:  Wang XJ;  Wang RX(王睿星);  Wang L;  Chen XJ;  Geng XY
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Non-probabilistic reliability based  multidisciplinary design optimization  Single loop strategy  Uncertainty multidisciplinary analysis  Non-probabilistic reliability analysis  Translating distance calculation