The stress distribution in shell bodies and wings as an equilibrium problem (1937)
NASA Technical Reports Server (NTRS) · leaf 28
N.A.C.A. Technical Memorandum No. 817 Figs.22,23,25 … VA? 9t°t Load a^ is not plotted ac- curately; it should run par- allel to the transverse line connecting the flanges, as readily seen in fig. 27. V5V
NASA Technical Reports Server (NTRS)
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