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A study of the pitching moments and the stability characteristics of monoplanes (1934)

NASA Technical Reports Server (NTRS) · leaf 17

An illustration from A study of the pitching moments and the stability characteristics of monoplanes, 1934, leaf 17 — H.A.O.A. Teonnioal Hote No. 511 rigure 2.- Angular relation of wing and tail. … Figure 1.- Pitching-moment diagram of low-wing or high-wing monoplane.

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