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At a point in a loaded components the state of stress is given by

$\sigma _{X}$ = 270 MPa ,   $\sigma _{y}$  = 130 MPa  and

$\tau _{XY}$  = Ā±40MPa

Determine

(i)   The maximum and minimum principal stresses and the planes on which they act.

(ii)  The maximum shearing stress in magnitude and direction

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