Method of determining approximately conditions in which it is necessary to automatically balance moment of propeller thrust by supplementary moment of empennage; determining rapidly best possible position of center of gravity to give sufficient stability without placing exaggerated stress on stabilizer and elevators; effect of slipstream of wing and propeller on fuselage.
Method of calculating the horizontal tail surfaces of an airplane
Abaque pour le calcul de l'empennage horizontal d'un avion
Aeronautique ; 11 , n 116
1929
8 pages
6 Figs.
Article (Journal)
French
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