Tests of 16 related airfoils at high speed
Description:
From Summary: "In order to provide information that might lead to the development of better propeller section, 13 related symmetrical airfoils were tested in the NACA high-speed wind tunnel for a study of the effect of thickness form on the aerodynamic characteristics. The thickness-form variables studies were the value of the maximum thickness, the position along the chord at which the maximum thickness occurs, and the value of the leading-edge radius. The tests were conducted through the low …
more
Date:
April 28, 1934
Creator:
Stack, John & von Doenhoff, Albert E.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department