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Torsional rigidity of cantilever wings with constant spar and rib sections (1929)

NASA Technical Reports Server (NTRS) · leaf 47

An illustration from Torsional rigidity of cantilever wings with constant spar and rib sections, 1929, leaf 47 — N.A.C.A. Technical Memorandum No.530 Figs.17 & 18 … 0 .1 .2 .3 .4 .5 .6 .7 .8 .9 1.0 Fig.18

NASA Technical Reports Server (NTRS)

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