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Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage (1933)

NASA Technical Reports Server (NTRS) · leaf 22

An illustration from Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage, 1933, leaf 22
N.A.O.A. Technical Note No.462 Table Table 71. Moment0, Axial Force, and Shear at Various Points in Bulkhead Ring No. 3 for the Loading Shown in Figs. 6 and 7. Axial Force (a) … (c) 4-i-33

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