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