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Airplane design and construction (1919)

Pomilio, Ottorino · New York, McGraw-Hill · leaf 342

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1000lb. is suddenly appUed upon the elevator. Let us note that the stresses thus calculated are greaterthan those had in practice; in fact for the calculation of theangular acceleration, the total moment of inertia of theairplane and not only that of the fuselage should havebeen introduced:… … /= H.H.Y= 100x50x19.4= 97.000 lb. mass. K in^ Fig. 197. 328 AllWLANE DESIGN AND CONSTRUCTION

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