Scale Effect on Clark Y Airfoil Characteristics from NACA Full-Scale Wind-Tunnel Tests (1935)
NASA Technical Reports Server (NTRS) · leaf 5
ormed by aluminum ribs spaced at 12-inch intervals. Access to the airfoil support pins was provided by 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… … Figure 2.—A tare-force set-up with inverted 6 by 3G airfoil.
NASA Technical Reports Server (NTRS)
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