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 1 L - L L Asymptote h Htf *" Figure 17.- Stress of outside fiber 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.-… … Figure 20.- Angle of Figure 21.- Shear stiffness of sheets displacement. "buckled under compressive stresses Op only.
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