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Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage (1933)
NASA Technical Reports Server (NTRS) · leaf 29
Figs. 8,9 N.A.C.A. Technical Hote Uo.462 2670 lb. [____ 2570 lb. … 10640 Lb. Figure 8.- Reinforced bulkhead ring th loads. 2200 lb. \ A */ / 4070 lb. 22C0 lb. 1 10840 lb. e -tt/2 (c) Case II (a) Case VI (b) Case. Ill (* 26^0 lb. 2570 lb. 2670 lb. X. /X \ ■H- V \ / I 9 = tt/2, f s -2670 lb. (f) (d) Case I (o) Case V Figure 9.- Loading sliov/n in figure 8 resolved…NASA Technical Reports Server (NTRS)
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