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188   •  Chapter 6    /    Mechanical Properties of Metals


            true strain         Furthermore, it is occasionally more convenient to represent strain as true strain P T ,
                                defined by

            Definition of true                               P T = ln   l i                        (6.16)
            strain                                                  l 0
                                If no volume change occurs during deformation—that is, if
                                                             A i  l i = A 0  l 0                   (6.17)

                                —then true and engineering stress and strain are related according to
            Conversion of
            engineering stress                             s T = s(1 + P)                         (6.18a)
            to true stress
            Conversion of                                                                         (6.18b)
            engineering strain                             P T = ln (1 + P)
            to true strain
                                Equations 6.18a and 6.18b are valid only to the onset of necking; beyond this point, true
                                stress and strain should be computed from actual load, cross-sectional area, and gauge
                                length measurements.
                                   A schematic comparison of engineering and true stress–strain behaviors is made in
                                Figure 6.16. It is worth noting that the true stress necessary to sustain increasing strain
                                continues to rise past the tensile point M¿.
                                   Coincident with the formation of a neck is the introduction of a complex stress state
                                within the neck region (i.e., the existence of other stress components in addition to the
                                axial stress). As a consequence, the correct stress (axial) within the neck is slightly lower
                                than the stress computed from the applied load and neck cross-sectional area. This leads
                                to the “corrected” curve in Figure 6.16.
                                   For some metals and alloys the region of the true stress–strain curve from the
                                onset of plastic deformation to the point at which necking begins may be approxi-
            True stress–true    mated by
            strain relationship in                                  n
            the plastic region of                            s T = KP T                            (6.19)
            deformation (to the
            point of necking)   In this expression, K and n are constants; these values vary from alloy to alloy and
                                also depend on the condition of the material (whether it has been plastically de-
                                formed, heat-treated, etc.). The parameter n  is often termed the strain-hardening
                                exponent  and has a value less than unity. Values of n  and K  for several alloys are
                                given in Table 6.4.




                                Figure 6.16  A comparison of typical
                                tensile engineering stress–strain and                         True
                                true stress–strain behaviors. Necking
                                begins at point M on the engineering              M           Corrected
                                curve, which corresponds to M¿ on
                                the true curve. The “corrected” true   Stress       M
                                stress–strain curve takes into account                     Engineering
                                the complex stress state within the neck
                                region.



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