A Rotary Wing System for Micro Air Vehicle Applications. Part 1
Journal Title: INCAS BULLETIN - Year 2011, Vol 3, Issue 3
Abstract
The goal of the paper is to propose a new type of ornithopter that avoids the mechanical difficulties of a flapping system. It uses a modified design of a cycloidal propulsor. The modification regards the special setting of the wings that is intended to help the formation of a stable leading edge vortex (LEV). It is known that the LEV is the main feature that allows the insects to achieve the necessary lift to fly.
Authors and Affiliations
Valentin BUTOESCU
Keywords
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- EP ID EP119246
- DOI 10.13111/2066-8201.2011.3.3.3
- Views 114
- Downloads 0
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