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Turbulent boundary layer of an airfoil (1937)
NASA Technical Reports Server (NTRS) · leaf 23
Figure 11.- Wing with Gottingen 39^ profile (t = 40 cm. a = 12°, x = 27.05 cm. T3 8 ="0.0075 m. r = 0.3278 kg/ra2; dp/ds = 283 Kg/m3.)NASA Technical Reports Server (NTRS)
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