Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil

Aerodynamics Study of Tubercle Effect on NACA4412 Airfoil The purpose of this research is to study the aerodynamics characteristics of NACA4412 airfoil with tubercle effect on its leading edge. The study was performed on three different leading edges of the airfoil; leading edge without the tuber...

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Main Author: Enso, Ennelyn Novema
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2017
Subjects:
Online Access:http://eprints.usm.my/51669/
http://eprints.usm.my/51669/1/Aerodynamics%20Study%20Of%20Tubercle%20Effect%20On%20NACA4412%20Airfoil_Ennelyn%20Novema%20Ensoh_A2_2017.pdf
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author Enso, Ennelyn Novema
author_facet Enso, Ennelyn Novema
author_sort Enso, Ennelyn Novema
building USM Institutional Repository
collection Online Access
description Aerodynamics Study of Tubercle Effect on NACA4412 Airfoil The purpose of this research is to study the aerodynamics characteristics of NACA4412 airfoil with tubercle effect on its leading edge. The study was performed on three different leading edges of the airfoil; leading edge without the tubercles, leading edge with spherical tubercles and leading edge with continuous spherical tubercles. The study focuses on the effect of the spherical tubercles on aerodynamics lift and drag characteristics of the NACA4412 airfoil. The experiment was performed by using the wind tunnel in the aerodynamics laboratory in Universiti Sains Malaysia. The result was obtained, compared and discussed further in the thesis.
first_indexed 2025-11-15T18:28:43Z
format Monograph
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institution Universiti Sains Malaysia
institution_category Local University
language English
last_indexed 2025-11-15T18:28:43Z
publishDate 2017
publisher Universiti Sains Malaysia
recordtype eprints
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spelling usm-516692022-02-25T08:18:46Z http://eprints.usm.my/51669/ Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil Enso, Ennelyn Novema T Technology Aerodynamics Study of Tubercle Effect on NACA4412 Airfoil The purpose of this research is to study the aerodynamics characteristics of NACA4412 airfoil with tubercle effect on its leading edge. The study was performed on three different leading edges of the airfoil; leading edge without the tubercles, leading edge with spherical tubercles and leading edge with continuous spherical tubercles. The study focuses on the effect of the spherical tubercles on aerodynamics lift and drag characteristics of the NACA4412 airfoil. The experiment was performed by using the wind tunnel in the aerodynamics laboratory in Universiti Sains Malaysia. The result was obtained, compared and discussed further in the thesis. Universiti Sains Malaysia 2017-06-01 Monograph NonPeerReviewed application/pdf en http://eprints.usm.my/51669/1/Aerodynamics%20Study%20Of%20Tubercle%20Effect%20On%20NACA4412%20Airfoil_Ennelyn%20Novema%20Ensoh_A2_2017.pdf Enso, Ennelyn Novema (2017) Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil. Project Report. Universiti Sains Malaysia, Pusat Pengajian Kejuruteraan Aeroangkasa. (Submitted)
spellingShingle T Technology
Enso, Ennelyn Novema
Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
title Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
title_full Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
title_fullStr Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
title_full_unstemmed Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
title_short Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
title_sort aerodynamics study of tubercle effect on naca4412 airfoil
topic T Technology
url http://eprints.usm.my/51669/
http://eprints.usm.my/51669/1/Aerodynamics%20Study%20Of%20Tubercle%20Effect%20On%20NACA4412%20Airfoil_Ennelyn%20Novema%20Ensoh_A2_2017.pdf