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Strength of Rectangular Flat Plates Under Edge Compression (1931)

NASA Technical Reports Server (NTRS) · leaf 9

An illustration from Strength of Rectangular Flat Plates Under Edge Compression, 1931, leaf 9
8 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS Strain, in/in. Figure 3—Stress-strain curves for duralumin. The thickness of the specunen is given on each curve. The yield point which is here defined as the stress for which the slope is one-third that of the modulus line is indicated by a… … Figure 4.—Stress-strain curves for stainless iron. Tlie thickness of the specimen is given on each curve. The yield point whicii is here defined as the stress for which the slope is one-third that of the modulus line is indicated by a short line crossing each curve \o.ooi^ Strain, in/in. Figure…

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