The state of stress at a point is given by: [ sigma_{x}=400 mathrm{MPa}, sigma_{y}=200 mathrm{MPa}, tau_{x y}=100

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The state of stress at a point is given by:

\[ \sigma_{x}=400 \mathrm{MPa}, \sigma_{y}=200 \mathrm{MPa}, \tau_{x y}=100 \mathrm{MPa}(\mathrm{ccw}) \]

Calculate the normal, shear and resultant stresses on a plane making an angle of \(30^{\circ}\) with the \(x\)-axis.

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