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全乘波背部进气高超声速飞机新概念构型研究 学位论文
博士论文，北京: 中国科学院大学, 2018
Authors:  肖尧
Adobe PDF(10334Kb)  |  Favorite  |  View/Download：933/20  |  Submit date：2018/05/24
高超声速飞行器  乘波体  背部进气布局  升阻比  气动设计与优化  
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
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Wang FM(王发民)
View  |  Adobe PDF(2721Kb)  |  Favorite  |  View/Download：626/141  |  Submit date：2018/06/16
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
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1937Kb)  |  Favorite  |  View/Download：281/90  |  Submit date：2018/10/30
Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration