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The stress distribution in shell bodies and wings as an equilibrium problem (1937)
NASA Technical Reports Server (NTRS) · leaf 24
N.A.C.JL. Technical Memorandum No. 817 Figs.1,3.3.4,5.6.7 Figure 4.- Advanced shell problem. Figure 7.- Membrane Figure 5.- Wing spar. Figure 6.- Shell "body. equilibrium.NASA Technical Reports Server (NTRS)
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