摘要
本文简述了机翼升力产生原理,提出了合理改变低速飞行器机翼表面摩擦系数分布可以适当增升、扑翼机可以在不同速度下用不同的扑翼方式改变升力的想法。以及下反角机翼比上反角机翼更稳定的观点。并进行了相关论述。
This paper briefly describes the principle of wing lift generation,the idea that changing the distribution of friction coefficient on the wing surface of low-speed aerocraft can increase the lift properly and that the flapping wing can change the lift in different ways at different speeds is put forward.And that the lower dihedral wing is more stable than the upper dihedral wing.And has carried on the related elaboration.
作者
徐崧
杨陆
李康
Xu Song;Yang Lu;Li Kang(Dalian Jiaotong University,Dalian Liaoning,116041)
出处
《电子测试》
2020年第17期137-138,共2页
Electronic Test
关键词
摩擦系数分布
扑翼方式
下反角
Friction Coefficient Distribution
flapping-wing mode
lower dihedral
