Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel
Description:
This report presents the results of an investigation conducted in the NACA full-scale wind tunnel to determine the aerodynamic characteristics of the 6 by 36-foot rectangular NACA 0025 and 0035 airfoils. The aerodynamic characteristics of the plain airfoils with rounded and square tips were determined by force tests through a complete angle-of-attack range; in addition, the profile drag was determined by the momentum method. The transition points on the airfoils were located by boundary-layer d…
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Date:
1941
Creator:
Bullivant, W. Kenneth
Item Type:
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