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...
Saved in:
Main Authors: | , , |
---|---|
Format: | Article |
Language: | English |
Published: |
Asian Research Publishing Network (ARPN)
2018
|
Subjects: | |
Online Access: | http://eprints.uthm.edu.my/4443/1/AJ%202018%20%28771%29.pdf http://eprints.uthm.edu.my/4443/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
id |
my.uthm.eprints.4443 |
---|---|
record_format |
eprints |
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 |
13.18916 |