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

NASA Technical Reports Server (NTRS) · leaf 26

An illustration from Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage, 1933, leaf 26
N.A.C.A. Technical Hote No.462 ng. 4 … Figors 4.- Sketch showing directions of moment, shear, axial force, and angular location assumed as positive in this report.

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