Experimental Studies of the Effective Width of Buckled Sheets (1936)
NASA Technical Reports Server (NTRS) · leaf 26
Figs, 5,6,7,9,11 N.A.C.A. Technical Memorandum No. 814 "]f" Figure 6.- Sheet Figure 5.- Owing -\ 1 1 H - with <-' to edge stiffeners. wrinkling the compressive stress drops at some distance from the edge stiffener to nearly zero. Figure 9.- Compression taken up by the sheet, \ ex- 50 100 10 » I M… … buckling lead is \ largely exceeded, \ 500 re*. 05 * J I J I L 200 vH b 100 o 50 100 cJtji J>00 1000 5 10 0^ ± Figure 7.- Illustration of the test Q510~3 data for effective width. Duralumin
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