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 rolling mo...

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Veröffentlicht in:	Aircraft Engineering 2010-01, Vol.82 (1), p.23-31
Hauptverfasser:	Elsayed, Omer A., Kwon, Kijung, Asrar, Waqar, Omar, Ashraf A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace industry Aircraft Aircraft hazards Angle of attack Coefficients Flight dynamics Flight operations Fluid dynamics Fluid flow Followers Lasers Mathematical models Reynolds number Rolling moments Studies Subsonic aircraft Swingwing aircraft Trailing edge flaps Velocity Velocity distribution Vortex generators Vortices Wings (aircraft)
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