Induced rolling moment for NACA4412 plain and flapped wing

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Induced rolling moment for NACA4412 plain and flapped wing

Purpose – The paper aims to compute rolling moments on a follower aircraft wing due to vortices generated by a plain and flapped NACA4412 wing using experimental particle image velocimetery (PIV) data. Design/methodology/approach – This paper describes the detailed variation of the induced rolli...

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Bibliographic Details
Main Authors:	Elsayed, Omer Ali, Kwon, Kijung, Asrar, Waqar, Omar, Ashraf Ali E.
Format:	Article
Language:	English
Published:	Emerald Group Publications Limited 2010
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/1969/ http://irep.iium.edu.my/1969/1/Induced_rolling%5B1%5D.pdf

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