Page 82 - 04. Subyek Engineering Materials - Manufacturing, Engineering and Technology SI 6th Edition - Serope Kalpakjian, Stephen Schmid (2009)
P. 82

Section 2.2  Tension

              situation: A specimen 50 mm in height is compressed between flat platens to a final
              height of zero; in other Words, We have deformed the specimen infinitely. According
              to their definitions, the engineering strain that the specimen undergoes  is
              (0 - 50)/50 = - 1, but the true strain is -OO. Note that the answer will be the same
              regardless of the original height of the specimen. Clearly, then, true strain describes
              the extent of deformation correctly, since the deformation is indeed infinite.


              2.2.4 Construction of Stress-Strain Curves
              The procedure for constructing an engineering stress-strain curve is to take the
              load-elongation curve (Fig. 2.5 a; also, Fig. 2.2), and then to divide the load (vertical
              axis) by the original cross-sectional area, AO, and the elongation (horizontal axis) by
              the original gage length,  IO. Because  AO and  lo are constants, the engineering
              stress-strain curve obtained (shown in Fig. 2.5b) has the same shape as the
              load-elongation curve shown in Fig. 2.5a. (In this example, AO = 36.1 mml and
              A/1= 10.3 mml.)



                   °¢                                 600
                    S2  2                          E?
                    ><
                    Q*                             § 400
                                                   §
                    ‘L_  1
                    Q                              5  200
                    O
                    _I
                        0                               0
                         0     10     20    30           0      0.2    0.4    0.6
                            Extension, A/ (mm)                   Strain (S)

                                   (G)                              (b)
                     1600

                           Maximum load
                   §`l2OO -             l,               4
                   E               ,,’  I
                   I            /' Corrected       A
                   Q 800 _          for necking    g
                                                   E
                   25
                   ‘U                              rn
                      400                          T5
                                                   G.)
                                                   |- E
                        O                             102
                         0     0.5    1.0   1.5         0.01      0.1       1.0
                              True strain (e)                  True strain (S)
                                   (C)                              (G)

              FIGURE 2.5  (a) Load-elongation curve in tension testing of a stainless steel specimen.
              (b) Engineering stress-engineering strain curve, drawn from the data in Fig. 2.5a. (c) True
              stress-true strain curve, drawn from the data in Fig. 2.5 b. Note that this curve has a positive
              slope, indicating that the material is becoming stronger as it is strained. (d) True stress-true strain
              curve plotted on log-log paper and based on the corrected curve in Fig. 2.5c. The correction is
              due to the triaxial state of stress that exists in the necked region of the specimen.
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