Calculation of load distribution in stiffened cylindrical shells (1938)
NASA Technical Reports Server (NTRS) · leaf 66
N.A.C.JL. Technical Memorandum No. 866 Figs.9,10,12,13 … Figure 9.- Stress condition due to applied convexing force group Xk = 1. a, Symmetrical with respect to center. ft ' s, b. Simply symmetrical Figure 10.- Section of a Figure 13.- Characteristic force circular groups for 12-stringer cylindrical shell. shell with doubly-symmetrical cross section.…
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