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Comparative study of turbulent incompressible flow past naca airfoils

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 thes...

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Main Authors: Abdullah, Aslam, Roslan, Amirul Aizad, Omar, Zamri
Format: Article
Language:English
Published: Asian Research Publishing Network (ARPN) 2018
Subjects:
TL500-777 Aeronautics. Aeronautical engineering
Online Access:http://eprints.uthm.edu.my/4443/1/AJ%202018%20%28771%29.pdf
http://eprints.uthm.edu.my/4443/
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spelling my.uthm.eprints.44432021-12-06T08:10:35Z http://eprints.uthm.edu.my/4443/ Comparative study of turbulent incompressible flow past naca airfoils Abdullah, Aslam Roslan, Amirul Aizad Omar, Zamri TL500-777 Aeronautics. Aeronautical engineering 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. Asian Research Publishing Network (ARPN) 2018 Article PeerReviewed text en http://eprints.uthm.edu.my/4443/1/AJ%202018%20%28771%29.pdf 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
institution Universiti Tun Hussein Onn Malaysia
building UTHM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tun Hussein Onn Malaysia
content_source UTHM Institutional Repository
url_provider http://eprints.uthm.edu.my/
language English
topic TL500-777 Aeronautics. Aeronautical engineering
spellingShingle TL500-777 Aeronautics. Aeronautical engineering
Abdullah, Aslam
Roslan, Amirul Aizad
Omar, Zamri
Comparative study of turbulent incompressible flow past naca airfoils
description 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.
format Article
author Abdullah, Aslam
Roslan, Amirul Aizad
Omar, Zamri
author_facet Abdullah, Aslam
Roslan, Amirul Aizad
Omar, Zamri
author_sort Abdullah, Aslam
title Comparative study of turbulent incompressible flow past naca airfoils
title_short Comparative study of turbulent incompressible flow past naca airfoils
title_full Comparative study of turbulent incompressible flow past naca airfoils
title_fullStr Comparative study of turbulent incompressible flow past naca airfoils
title_full_unstemmed Comparative study of turbulent incompressible flow past naca airfoils
title_sort comparative study of turbulent incompressible flow past naca airfoils
publisher Asian Research Publishing Network (ARPN)
publishDate 2018
url http://eprints.uthm.edu.my/4443/1/AJ%202018%20%28771%29.pdf
http://eprints.uthm.edu.my/4443/
_version_ 1738581251100508160
score 13.211869

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