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基于流线追踪的变截面进气道快速设计 学位论文
北京: 中国科学院大学, 2018
作者:  肖鸿文
收藏  |  浏览/下载:62/0  |  提交时间:2018/05/28
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
作者:  Xiao YB(肖雅斌);  Yue LJ(岳连捷);  Ma SH;  Zhang XY(张新宇)
收藏  |  浏览/下载:27/0  |  提交时间:2016/09/14
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
收藏  |  浏览/下载:27/0  |  提交时间:2014/02/24


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