Strength Tests of Thin-walled Duralumin Cylinders in Pure Bending (1933)
NASA Technical Reports Server (NTRS) · leaf 16
/6 N.A.C.A. Technical Note No. 479 Fig. 6 … 100 600 800 1,000 1,400 2,000 200 400 Radius r ■ I T Thickness t A, Robertson cylinders; graph of equation(6), reference 2, with 6 E " V3(l-o2) r B, Cylinders of infinite length; graph of equation(8), reference 2, with a - 0.3, ■ °'6J^JJ^J £ C, Lower limit of test data. Figure 6.-Logarithmic plot…
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