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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Bibliographic Details
Main Author: Ng, Bing Feng.
Other Authors: Jorg Uwe Schluter
Format: Final Year Project
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/16798
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Institution: Nanyang Technological University
Language: English

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