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Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps (1937)

NASA Technical Reports Server (NTRS) · leaf 25

An illustration from Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps, 1937, leaf 25 — W.A.C.A. Technical Note llo. 597 … Hinge-moment coefficient. Figure 6.- Effect of trimming tab setting on elevator hinge-moment coefficient (reference 7). If

NASA Technical Reports Server (NTRS)

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