Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage (1933)
NASA Technical Reports Server (NTRS) · leaf 25
N.A.C.A, Technical ITote ITo.4S2 Pigs. 2,3 2830 lb. 2830 Id. … Figure 2.~ Bulkhead ring Ho.2 of "Fleetster" airplane with symmetrical loading. W2 = 2830 1c. Y?2 ■ 2830 l'b. \ / - CJ \ -x- • Wf T w3 - 15230 j s-—| 15230 15100 lb. 1 15100 lb. | lb. W3 = 15200 If. •2 = 2330 To. Wg = 2S3C (b) Case I To. (c) Case II (a) Case VI with W = -2830 It. with W = -15280…
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