Aerodynamic Design and Exploration of a Blended Wing Body Aircraft at Subsonic Speed

被引：0
|
作者：
Dakka, Sam [1 ]
Johnson, Oliver [2 ]
机构：
[1] Univ Nottingham, Nottingham, England
[2] Sheffield Hallam Univ, Sheffield, S Yorkshire, England
来源：
INTERNATIONAL JOURNAL OF AVIATION AERONAUTICS AND AEROSPACE | 2019年 / 6卷 / 05期
关键词：
31;
D O I：
10.15394/ijaaa.2019.1411
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页数：31
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