Engineering strain is a measure of deformation relative to a material's original size. It is defined as the change in length divided by the original length ($L_0$).
The formula for engineering strain ($\epsilon$) is:
$ \epsilon = \frac{\Delta L}{L_0} = \frac{L_{final} - L_0}{L_0} $
The problem states:
Calculate the final length after extension ($L_1$):
$L_1 = 2 \times L_0 = 2 \times 2 \text{ cm} = 4 \text{ cm}$.
Calculate the change in length during extension ($\Delta L_{ext}$):
$\Delta L_{ext} = L_1 - L_0 = 4 \text{ cm} - 2 \text{ cm} = 2 \text{ cm}$.
Calculate the engineering strain for the extension phase ($\epsilon_{ext}$):
$ \epsilon_{ext} = \frac{\Delta L_{ext}}{L_0} = \frac{2 \text{ cm}}{2 \text{ cm}} = 1 $
After extension, the element's length is $L_1 = 4$ cm.
The element is then compressed back to its initial length ($L_0 = 2$ cm). Let the final length after compression be $L_2$. So, $L_2 = 2$ cm.
Calculate the change in length during compression ($\Delta L_{comp}$):
$\Delta L_{comp} = L_2 - L_1 = 2 \text{ cm} - 4 \text{ cm} = -2 \text{ cm}$.
Calculate the engineering strain for the compression phase ($\epsilon_{comp}$). The reference length (original length for this step) is the length before compression, which is $L_1 = 4$ cm.
$ \epsilon_{comp} = \frac{\Delta L_{comp}}{L_1} = \frac{-2 \text{ cm}}{4 \text{ cm}} = -0.5 $
The engineering strains for the extension and compression are 1 and -0.5, respectively.
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