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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 6

An illustration from Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle, 1936, leaf 6 — N.A.C.A. Technical Note No. 552 Fig. 1 tn t+ «7t- O .wo i>-700 0 .386 g^.1>090 .25 . 50

NASA Technical Reports Server (NTRS)

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