摘要
在研究鸟飞行机制的基础上,通过对扑翼飞行翅的简化和分析,建立了仿生扑翼飞行的简化力学模型,结合翼形导出了在一个扑动周期中翅上所产生的平均前进力和升力公式。实验证明了该简化力学模型及相应力学分析的可靠性和正确性。研究成果为进一步研制仿生扑翼飞行器提供了理论依据。
Researching on the bird flight mechanism,a simple mechanics model of flapping-wing flight was established by analyses of the flapping-wing. The formulas of the average drag and lift force, which combined the wing shape, were derived during one period. The experimental results show that the simple mechanics model and mechanics analysis are reliable and feasible. The research outcomes will offer the theoretical foundation for further research.
出处
《中国机械工程》
EI
CAS
CSCD
北大核心
2007年第6期631-634,共4页
China Mechanical Engineering
基金
江苏省高校自然科学基金资助项目(02KJD460010)
关键词
扑翼飞行
仿生学
力学模型
实验
flapping- wing flight
bionics
mechanics model
experiment
