Browsing Mechanical and Mechatronics Engineering by Subject "NACA 0018 airfoil"
Now showing items 1-1 of 1
(University of Waterloo, 2011-07-27)Shear layer development over a NACA 0018 airfoil at a chord Reynolds number of 100,000 was investigated experimentally. The effects of experimental setup and analysis tools on the results were also examined. The sensitivity ...