1) The relative change in length (contraction) is
"\\epsilon=\\frac{L_0-L}{L_0}=\\frac{L_0-L_0(1+\\alpha\\Delta T)}{L_0},\\\\\\space\\\\\n\\epsilon=\\frac{L_0-L_0(1+\\alpha(-20-70))}{L_0}=1.53\u00b710^{-3}." The stress is
"\\sigma=E\\epsilon=(210\u00b710^9)(1.53\u00b710^{-3})=321.3\u00b710^6\\text{ Pa}." This is axial stress.
2) The equation for the heat supplied is
"Q=cm(T_f-T_i),\\\\\\space\\\\\nT_f=\\frac{Q}{cm}+T_i=\\frac{1000}{460\u00b70.01875}+20=136\u00b0\\text C."
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