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The balance of moments and the static longitudinal stability of airplanes (1929)

NASA Technical Reports Server (NTRS) · leaf 16

An illustration from The balance of moments and the static longitudinal stability of airplanes, 1929, leaf 16 — Fig-8 … Tail lift coef f icient, c.,h 0..5 . \, ""^0 1.0 1:10 Tail angle of attack,aJJ ^-^g^j. Fig.8 Stability nomogram.

NASA Technical Reports Server (NTRS)

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