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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Universiti Sains Malaysia
2017
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my.usm.eprints.51669 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) |
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T Technology Enso, Ennelyn Novema Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil |
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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. |
format |
Monograph |
author |
Enso, Ennelyn Novema |
author_facet |
Enso, Ennelyn Novema |
author_sort |
Enso, Ennelyn Novema |
title |
Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil |
title_short |
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_sort |
aerodynamics study of tubercle effect on naca4412 airfoil |
publisher |
Universiti Sains Malaysia |
publishDate |
2017 |
url |
http://eprints.usm.my/51669/1/Aerodynamics%20Study%20Of%20Tubercle%20Effect%20On%20NACA4412%20Airfoil_Ennelyn%20Novema%20Ensoh_A2_2017.pdf http://eprints.usm.my/51669/ |
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13.18916 |