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Calculation of load distribution in stiffened cylindrical shells (1938)

NASA Technical Reports Server (NTRS) · leaf 67

An illustration from Calculation of load distribution in stiffened cylindrical shells, 1938, leaf 67
Figs. 14,15,16,1? 2T.A.C.A. Technical Memorandum Ho. 866 6-bay shell --■ All bulkheads elastic. Infinite- … Bulkhead number k number k Figure 14.- Falling off of applied Figure 15.- Effect of the various convexing force group stiffnesses on the Xo = 1 over shell length. distribution of the applied force group X0 = 1. Figure 16.- Falling off of simply- b, Effective redundant force groups symmetrical…

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