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Alternative TitleAerodynamic testing system for air vehicle with micro flapping wings
李贵祥; 苏刚; 李洪谊
Source Publication机械设计与制造
Contribution Rank1
Funding Organization863基金项目(09H1230101)
Keyword扑翼 气动力 测试系统
Other AbstractThe aerodynamic force is main performance index of air vehicle with micro flapping wings during flight,while the aerodynamics at low Reynolds number condition is not a mature theory,and has not empirical formula to follow,so an aerodynamic testing system of air vehicle with micro flapping wings is designed and verified:The system uses 2 force sensors located in parallel and vertical as the sensors to measure the thrust and the lift during flying of the air vehicle,and two flexible hinges are used to separate vertical and horizontal aerodynamic force as well as reduce the effect of force in non-force direction on force sensor.At last,the thrust and lift obtained from the system for testing aerodynamic force of the air vehicle with micro flapping wings is given and analyzed.
Document Type期刊论文
Recommended Citation
GB/T 7714
李贵祥,苏刚,李洪谊. 微型扑翼飞行机器人气动力测试系统[J]. 机械设计与制造,2012(2):165-167.
APA 李贵祥,苏刚,&李洪谊.(2012).微型扑翼飞行机器人气动力测试系统.机械设计与制造(2),165-167.
MLA 李贵祥,et al."微型扑翼飞行机器人气动力测试系统".机械设计与制造 .2(2012):165-167.
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