The state of plane stress at a point on a body is represented by the element below.

 Angle: $\theta =$ {{theta}} $^o$ Normal stress ($\sigma_x$): $\sigma_x =$ {{sigmax}} $MPa$ Normal stress ($\sigma_y$): $\sigma_y =$ {{sigmay}} $MPa$ Shear stress ($\tau_{xy}$): $\tau_{xy} =$ {{tauxy}} $MPa$