Scale Effect on Clark Y Airfoil Characteristics From NACA Full-Scale Wind-Tunnel Tests
Description:
This report presents the results of wind tunnel tests conducted to determine the aerodynamic characteristics of the Clark Y airfoil over a large range of Reynolds numbers. Three airfoils of aspect ratio 6 and with 4, 6, and 8 foot chords were tested at velocities between 25 and 118 miles per hour, and the characteristics were obtained for Reynolds numbers (based on the airfoil chord) in the range between 1,000,000 and 9,000,000 at the low angles of attack, and between 1,000,000 and 6,000,000 at…
more
Date:
June 14, 1934
Creator:
Silverstein, Abe
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department