Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage (1933)
NASA Technical Reports Server (NTRS) · leaf 27
Figs. 5,6 N.A.C.A. Technical Note No.462 A090 lb, 3519 lb. 12304 lb. Or f i W 1 … Figure 5.- Bul'diead ring No. 3 of "Fleetster" airplane with unsymraetrical loading. 2W7 = 390 l"b. w2 = w2 = Wi ■ 4232 lb. 4392 Id. 7912 lb. 7912 lb. 1. 4^ ! k G E' \ Ok ! ' ^ c x 1 it . -c{|t-> \ ,c«- c«- c '•• C i __ 1 *si \ / I /J W2 = \/ -4- 1392 lb. '--4-'" 4392 Id. f3 a ***H-~~ Wg - I 445…
NASA Technical Reports Server (NTRS)
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