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...
Saved in:
| Main Author: | |
|---|---|
| Format: | Final Year Project |
| Language: | English |
| Published: |
Universiti Teknologi Petronas
2008
|
| Subjects: | |
| Online Access: | http://utpedia.utp.edu.my/648/1/Ahmad_Khairuddin_bin_Ahmad_Kamal.pdf http://utpedia.utp.edu.my/648/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Be the first to leave a comment!