Development and testing of a variable-spam morphing wing

The present work focuses on the development and validation of a variable-span morphing wing (VSW) to be fitted to a mini UAV. An electro-mechanical actuation mechanism is developed using a simple rack and pinion system. The wing model is designed with the help of graphical CAD/CAE tools and then a f...

Full description

Bibliographic Details
Main Author: Felício, João Miguel Inácio (author)
Format: masterThesis
Language:eng
Published: 2015
Subjects:
Online Access:http://hdl.handle.net/10400.6/3663
Country:Portugal
Oai:oai:ubibliorum.ubi.pt:10400.6/3663