Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil

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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Bibliographic Details
Main Author: Enso, Ennelyn Novema
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2017
Subjects:
T Technology
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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