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Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs (1939)

NASA Technical Reports Server (NTRS) · leaf 13

An illustration from Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs, 1939, leaf 13 — I.A.C.A. Tecanloal Vote Ho. 734 Figure 4.- Distribution of resultant pressure ovar the S.k.Q.k. 0009 airfoil at various angles of attaok. Tlap and tab neutral.

NASA Technical Reports Server (NTRS)

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