Correct Answer - Option 3 : 2τ sin 45°cos 45°
Concept:
For biaxial stress accompanied by simple shear stress at any plane then,
Maximum principal stress is
\({{\rm{σ }}_{\rm{p}}} = \frac{{{{\rm{σ }}_{\rm{x}}} + {{\rm{σ }}_{\rm{y}}}}}{2} - \frac{{{{\rm{σ }}_{\rm{x}}} - {{\rm{σ }}_{\rm{y}}}}}{2}\cos 2{\rm{θ }} - {{\rm{τ }}_{{\rm{xy}}}}\sin 2{\rm{θ }}\)
when there is the normal stress in a plane which is inclined at an angle θ with the horizontal axis;
σx and σy are the normal stress in the direction of the X-axis and Y-axis respectively;
τxy is the shear stress acting in the XY plane.
Tensile normal stress is taken as positive, compressive normal stress is taken as negative.
Calculations:
Given:
It is a pure shear stress case
σx = σx = 0 and τxy = τ and θ = 45°
Maximum principal stress:
\({{\rm{σ }}_{\rm{p}}} = \left(\frac{{0 + 0}}{2}\right) - \left(\frac{{0 - 0}}{2}\right)\cos (2 \times 45) - {\rm{τ }} \times \sin (2 \times 45^{\circ}) \)
σp = τ sin2 45° .....................(Clockwise shear stress is taken as positive along the x-x axis)
σp = 2τ sin 45°cos 45° ........(sin 2θ = 2 sinθcosθ)
∴ The resulting normal stress (tensile or compressive) on planes inclined at 45° to the direction of the shear stresses is equal to τ.