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...

Full description

Saved in:
Bibliographic Details
Main Author: Enso, Ennelyn Novema
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2017
Subjects:
Online Access: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/
Tags: Add Tag
No Tags, Be the first to tag this record!
Be the first to leave a comment!
You must be logged in first