Calculation of load distribution in stiffened cylindrical shells (1938)
NASA Technical Reports Server (NTRS) · leaf 68
Figs. 18,19,20,21,22 N.A.C.A. Technical Memorandum No, 866 Simplified Ttesf values … Figure 18.- Force distribution in Figure 19.- Comparison of computed the simplified shell and measured stringer due to the bending force group stresses due to the bending force group. Z f2-3,S3cm2 Solution for equal bays .from elasticity; equations l-> TBulkheads Independent ^ -/elastic difference…
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