Fluid-structure interactions of variable span wings in low Reynold flows

Salleh, Hafiz and Saharin, Sanisah and Azmi, Mohammad Hanafi and Khan, Sher Afghan (2018) Fluid-structure interactions of variable span wings in low Reynold flows. International Journal of Engineering & Technology, 7 (3.29). pp. 381-385. ISSN 2227-524X

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Abstract

Numerical method is one of the method which is applied to study the aerodynamics of static variable span morphing wing and to evaluate flow structure over the wing surface (especially leading edge) at different low reynolds number/flow. The numerical result of lift coefficient vs span increment (pencentage) is validated with experimental result from previous study. Effect of the change of wingspan on low Reynold number/flows is investigated for the wing lift coefficient, and aerodynamics efficiency. Some contour results including pressure contour is observed. The pressure contour along wingspan from each case is figured out.

Item Type:	Article (Journal)
Additional Information:	4865/66198
Uncontrolled Keywords:	Morphing Wing; Variable Span Wing; Low Reynold
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering Kulliyyah of Engineering
Depositing User:	Prof. Dr. Sher Afghan Khan
Date Deposited:	02 Oct 2018 14:27
Last Modified:	02 Oct 2018 14:27
URI:	http://irep.iium.edu.my/id/eprint/66198

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