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Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle (1936)

NASA Technical Reports Server (NTRS) · leaf 8

An illustration from Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle, 1936, leaf 8 — 1 … Figure 3.- Polar curvee for wing with flap at position 0 1. Slot 5 D.

NASA Technical Reports Server (NTRS)

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