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Wrinkling of reinforced plates subjected to shear stresses (1931)
NASA Technical Reports Server (NTRS) · leaf 63
N.A.C.A. Technical Memorandum No.602 Figs.5a,5b 30 Curve e,rigid restraint … 0 40 to To 1/5 1/3 1/2 1 20 co^q 10 5 3 2 1 Fig. 5a ca plotted against 1/& within range of 0 = l/S- = 1 30 20 10 0 .04 0.25 0.50 0.75 1 1/5 1/2 1 Fig.5b cb plotted against £2 within range of 0 = £2 = 1NASA Technical Reports Server (NTRS)
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