Tests for the determination of the stress condition in tension fields (1936)
NASA Technical Reports Server (NTRS) · leaf 18
N.A.C.A. Technical Memorandum No, 809 Figs. 16,17,18,19,20,21 … of sheet midway between Figure 16.- Effective width in shear, two uprights. i Figure 18.- Cumulative stress E in each flange due to sheet tension. <3» -Oo 9» Figure 19.- Flange Bending moments. ^3 At* •<?« mnnninp II nnjnn fooo ft? it -~r- i|i|i|i|i|mijmr ||||||||||IIII|ITTT ll| I I 11| IIHfTTT…
NASA Technical Reports Server (NTRS)
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