Oblique flying wing supersonic airliner aerodynamic configuration parameters selection method

被引：0
|
作者：
机构：
[1] Hu, Shuyao
[2] Jiang, Chongwen
[3] Gao, Zhenxun
[4] Lee, Chunhian
来源：
Hu, S. (hshy1031@163.com) | 1600年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 40期
关键词：
Compendex;
D O I：
10.13700/j.bh.1001-5965.2013.0291
中图分类号：
学科分类号：
摘要：
Conceptual design
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