Calculation of load distribution in stiffened cylindrical shells (1938)
NASA Technical Reports Server (NTRS) · leaf 67
Figs. 14,15,16,1? 2T.A.C.A. Technical Memorandum Ho. 866 6-bay shell --■ All bulkheads elastic. Infinite- b, End bulkhead ly long < shell rigid. _ c, All bulkheads rigid. Thin liner: limiting case of sheet rigid in shear. Bulkhead Bulkhead number k number k Figure 14.- Falling off of applied Figure… … Figure 16.- Falling off of simply- b, Effective redundant force groups symmetrical character- Figure 17.- Bending force groups istic force group T0 = 1 over applied to the shell length. test shell.
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