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Standardization Tests of NACA No. 1 Wind Tunnel (1925)
NASA Technical Reports Server (NTRS) · leaf 13
Airfoil 7.5X'45cm. — Nominal speed IBmjsec- \ Nominal speed IBmlsec. E=0.632x10q= 16.65 kg/m ^ q=9.545kg/m E=0.520xl0-s 1.0 0.8 0.6 L 0.4 0.2 0.0 O-Erecf Inverted I I \ I \ L ^'X)0 .02 .04 ^ .06 .06 .10 Fig. 15. Fig. 13. Q> Airfoil 7.5x45 cm. Nominal speed 35m/sec.—I ^5m/se E= 1.716x10a= 78.00kQIm^… … Polars for U. S. A. IG airfoils.NASA Technical Reports Server (NTRS)
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