摘要
通过有限元软件分析飞翼布局飞机特有的翼梁受力特性,并与传统布局翼梁的受力特性进行对比,研究飞翼布局翼梁结构的应力特点,对今后飞翼布局飞机翼梁研究设计提供参考。
Characteristics of airfoil of flying wing aircrafts is analyzed using the finite element software. Compared withthe characteristics of airfoil of the traditional aircrafts, the stress characteristics of the wing structure of the flying wingaircrafts are studied. The results can provide reference for the future design of the flying wing aircrafts.
出处
《机械工程师》
2017年第12期121-122,125,共3页
Mechanical Engineer
关键词
飞翼布局
特性分析
flying wing aircrafts
characteristic analysis