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 Figure 22.- The compara- tive curved tension field. Figure 23.- Stress in cylin- drical shell be- tween two rings. Figure 25.- Cutout in torsion- ally stressed cylindrical shell. ■M r b m c
NASA Technical Reports Server (NTRS)
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