Morphing Wing Concept for Small UAV-Reference-Cited by-同舟云学术

Morphing Wing Concept for Small UAV

Published:2013-07 Issue: Volume:332 Page:44-49
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Prisacariu Vasile¹,Boşcoianu Mircea²,Cîrciu Ionică²^ORCID

Affiliation:

1. Henri Coanda Air Force Academy

2. "Henri Coandă" Air Force Academy

Abstract

The biological flight involves the movement of a wing (lift surface) in viscous medium and it generates lift and resistance for going forward through friction compared to Reynolds number. The morphing concept is generally based on optimizing the aerodynamic form during the mission so it can execute a maneuver flight. This article desires a short passage through the mathematical aspect in 2D of the morphing profile concept.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.332.44.pdf

Reference13 articles.

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4. Bourdin, P. Gatto, A. and Friswell, M.I. The Application of Variable Cant Angle Winglets for Morphing Aircraft Control, 24th Applied Aerodynamics Conference, 5 - 8 June 2006, San Francisco, California.

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