Design of tail unit and fuselage. (See also - vol. 20, nos. 399, 400 and 402, June 9, 16 and 30, 1921, pp. 415-417, 432-435 and 475-477, 21 figs)
The loads and stresses in aeroplanes
Aeronautics
Aeronautics ; 21 , n 406
1921
3 pages
4 Figs.
Article (Journal)
English
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The loads and stresses on aeroplanes
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