Aerodynamics of unconventional airfoils

Aerodynamics of unconventional airfoils

This project will explore lift enhancement methods for MAVs under low Reynolds number flight where CLmax are significantly lower. It will study the beneficial effects of vortices to enhance lift through both Static and Dynamic Leading Edge Vortices (LEVs). LEVs create an area of suction which genera...

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書目詳細資料
主要作者:	Ng, Bing Feng.
其他作者:	Jorg Uwe Schluter
格式:	Final Year Project
語言:	English
出版:	2009
主題:	DRNTU::Engineering::Mechanical engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics
在線閱讀:	http://hdl.handle.net/10356/16798
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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