Find stress:
"\\sigma=\\frac FA." Find strain:
"\\epsilon=\\frac{\\Delta l}{l}." Write the relation between srtress and strain:
"\\sigma=E\\epsilon=E\\frac{\\Delta l}{l},\\\\\\space\\\\\nE\\frac{\\Delta l}{l}=\\frac FA.\\\\\\space\\\\\n\nF=EA\\frac{\\Delta l}{l}=(2\u00b710^{11})\\bigg(\\frac\\pi 4(1^2-0.08^2)\\bigg)\\bigg(\\frac{0.1}{3.6}\\bigg)=\\\\\\space\\\\=4.34\u00b710^6\\text{ N}."
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