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: | , , , |
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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/ http://irep.iium.edu.my/1969/ http://irep.iium.edu.my/1969/ http://irep.iium.edu.my/1969/1/Induced_rolling%5B1%5D.pdf |