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The effect of small variations in profile of airfoils (1931)
NASA Technical Reports Server (NTRS) · leaf 13
Fig. 4 H.A.O.A. T3C-inical K'Ote ITo. 3ol Gottin;;3n 307 … 4 8 12 16 ~4 0 -8 Angle of attack, oc Fig. 4 Comparative curves for Gottingen 387-G & Gottingen 337. R.i:I. = 3.4 ^^lOS. Corrected to aspect ratio 6 in free air.NASA Technical Reports Server (NTRS)
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