CFD Simulation and Wind Tunnel Test of NACA 4412 Airfoil Wing Section at Different Angles of Attack
Airfoil can be defined as a body shape so that lift can be generated as fluid flow through it. The study of thin aerofoil by changes in a few characteristic such as different angle of attack, α would provide changes in lift, drag, and pitching moment coefficients. In order to identify the changes, C...
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Main Author: | Ahmad Khairuddin bin Ahmad Kamal, Ahmad Khairuddin |
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Format: | Final Year Project |
Language: | English |
Published: |
Universiti Teknologi Petronas
2008
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Subjects: | |
Online Access: | http://utpedia.utp.edu.my/648/1/Ahmad_Khairuddin_bin_Ahmad_Kamal.pdf http://utpedia.utp.edu.my/648/ |
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