True stress and true strain
The stress was calculated by dividing the load
P by the initial cross section of the specimen. But it is clear that as the
specimen elongates its diameter decreases and the decrease in cross section is
apparent during necking phase. Hence, the actual stress which is obtained by
dividing the load by the actual cross sectional area in the deformed specimen
is different from that of the engineering stress that is obtained using
undeformed cross sectional area as in equation 1.1 Though the difference
between the true stress and the engineering stress is negligible for smaller
loads, the former is always higher than the latter for larger loads.
Similarly, if the initial length
of the specimen is used to calculate the strain, it is called engineering
strain as obtained in equation 1.9
But some engineering applications
like metal forming process involve large deformations and they require actual
or true strains that are obtained using the successive recorded lengths to
calculate the strain. True strain is also called as actual strain or natural
strain and it plays an important role in theories of viscosity.
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