The principal strains in a plane, measured experimentally at a point on the 2014 T6 aluminum fuselage of a jet aircraft, are ( epsilon 1 450 left(10 6 ight) ) and ( epsilon 2 600 left(10 6 ight) ) Determine the associated principal stresses at the point in the same plane ...

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The principal strains in a plane, measured experimentally at a point on the 2014-T6 aluminum fuselage of

Question:

The principal strains in a plane, measured experimentally at a point on the 2014-T6 aluminum fuselage of a jet aircraft, are $\epsilon_{1}=450\left(10^{-6}\right)$ and $\epsilon_{2}=-600\left(10^{-6}\right)$. Determine the associated principal stresses at the point in the same plane.

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