Performance analysis of aerofoil for Unmanned Aerial Vehicle

被引：0
|
作者：
Faisal, Kh Md [1 ]
Papon, Md Easir Arafat [1 ]
Nafi, Akhter Mahmud [1 ]
机构：
[1] Mil Inst Sci & Technol, Dept Aeronaut Engn, Dhaka, Bangladesh
来源：
2014 1ST INTERNATIONAL CONFERENCE ON ELECTRICAL ENGINEERING AND INFORMATION & COMMUNICATION TECHNOLOGY (ICEEICT 2014) | 2014年
关键词：
Aerofoil; UAV; Drag; Lift co-efficient; pitching moment; lift-drag ratio;
D O I：
暂无
中图分类号：
TP301 [理论、方法];
学科分类号：
081202 ;
摘要：
The growing interest in development of UAV has created a need for the comparative analysis of performance parameters of different aerofoils. Using this concept different characteristics of aerofoils are explored to design the wing of various UAV fulfilling various purposes. In this research work, the requirements of our desired UAV are established. These requirements are translated into performance parameters. Then the aerofoil that best meet the requirements was optimized from different arbitrary aerofoils through experimental investigation of the performance parameters.
引用
收藏
页数：5
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