Formula for computing loads that come upon machine as a whole under various conditions of flight. Equations of equilibrium when flying and when alighting with engine shut off; approximate method of calculating loads when turning in horizontal position and when flattening out from vertical dive and looping. How flattening out of flight path is brought about. Loads caused by gusts, spiral glides and spinning. Distribution of load over the planes. Pressure distribution in spiral guide. (See also - vol. 16, nos. 289 and 291, 293, 294, 295, 296 and 297, May 1, 15, 29, June 5, 12, 19 and 26, 1919, pp. 556-559, 589-592, 619-622, 644-647 and 671-673, 32 figs)
The loads and stresses on aeroplanes
Aeronautics
Aeronautics ; 17 , n 300
1919
3 pages
4 Figs.
Article (Journal)
English
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