Aerodynamic improvement of a delta wing in combination with leading edge flaps

Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been reported from wide range points of view. The aim of this study is to research the aerodynamic improvement of delta wing in low Reynold’s number region to develop an applicative these air vehicle. As an attr...

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Bibliographic Details
Main Authors: Tadateru Ishide, Mao Itazawa
Format: Article
Language:English
Published: Elsevier 2017-11-01
Series:Theoretical and Applied Mechanics Letters
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2095034917301356