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Pressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight (1939)
NASA Technical Reports Server (NTRS) · leaf 8
N.A.C.A. Technical Note No. 735 Fig. 2a -3.0 Chore, 1 Chcrd ore Oqtei sjan -2.0 5 ■1.0 r L zz 1.0 p "To -3.0 … o Upper surface x Lower surface -2.0 1.0 J? -3.0 -2.0 -1.0 0 ,(a) The 25-peroent-span flap. Figures 2a to c- Pressure-distribution plots for 5° pitch, 0° yaw, flaps de- flected 60°.NASA Technical Reports Server (NTRS)
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