Comparative study of turbulent incompressible flow past naca airfoils

Abdullah, Aslam and Roslan, Amirul Aizad and Omar, Zamri (2018) Comparative study of turbulent incompressible flow past naca airfoils. ARPN Journal of Engineering and Applied Sciences, 13 (21). pp. 8527-8530. ISSN 1819-6608

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Abstract

The flow past the airfoils is continuously investigated in various experimental and computational aerodynamic perspectives. In this paper, a comparative study on the aerodynamic characteristics of the turbulent incompressible flow past four NACA airfoils is emphasized. Particularly, we classify these characteristics based on the basic geometries, namely symmetric and asymmetric airfoils, as well as trailing edge angles. The results confirm the general aerodynamic theory and include finding on the effect of sharp trailing edge, which complement the available airfoil datasets for improving their designs and as reference cases.

Item Type: Article
Uncontrolled Keywords: NACA airfoils; symmetric airfoils; unsymmetric airfoils; sharp trailing edge; turbulent incompressible flow
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500-777 Aeronautics. Aeronautical engineering
Divisions: Faculty of Mechanical and Manufacturing Engineering > Department of Aeronautical Engineering
Depositing User: UiTM Student Praktikal
Date Deposited: 06 Dec 2021 08:10
Last Modified: 06 Dec 2021 08:10
URI: http://eprints.uthm.edu.my/id/eprint/4443

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