Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle (1936)
NASA Technical Reports Server (NTRS) · leaf 13
I I CO … c o 4 6f b eo° + 6f = 40c 0 4 si o 1.91 1.85 1.75 1.28 f-\ 1.81 1.80 1.74 ti 14 + + + 1+ + 4- 4 (D EH 1,71 1.69 4- 4 2 4 4 4 4 2-1- + A B A> 0 A B A' « 0 o ■ Figaro 8.- Cj, against flap hinge axis location for flap deflections of 20°,40°,60°,and 80°. Slot 6. IDS *■
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