Scale Effect on Clark Y Airfoil Characteristics from NACA Full-Scale Wind-Tunnel Tests (1935)
NASA Technical Reports Server (NTRS) · leaf 5
REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS EQUIPMENT AND AIRFOILS Number range from about 1,000,000 to 9,000,000, The N.A.C.A. full-scale wind tunnel and equipment although data were not secured above a Reynolds are described in reference 2. Since the general equip- Number of about… … Figure 1.—The 6 by 36 airfoil mounted in the full-scale tunnel. removable plates which were screwed flush with the surface during the tests. Tapped openings for fitted fication of the theoretical jet-boundary correction for eyebolts were spaced over the airfoil for attachments the elliptical-jet…
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