Stress state:   s_x , s_y , t_xy 

   Angle of Rotation:         q      

   Transformed:     s_x' , s_y' , t_xy ;   In-Plane Principal:  s_I at q_I , s_II at q_II ;

   Max. In-Plane Shear:  +|t_max| on q_s1 , –|t_max| on q_s2 , s_ave ;

   Max. Out-of-Plane Shear:  t_max ;   von Mises stress:  s_o

1. Enter the original STRESSES on the element:
     s_x =    s_y =    t_xy =  

2. Enter the counterclockwise (positive) rotation of the element:
            q (degrees) = °   (leave as zero if only calculating max. values)

3. 

Stresses in rotated system (rotated q from original axis):

   s_x' =    s_y' =    t_x'y' =

Note: The angles listed below correspond to vectors (rotated q from the x-axis) that are normal to the faces on which the stresses act. Angles in degrees.

Principal Stresses
      Max. Principal Stress:  s_I =   at  q_I  = °
      Min. Principal Stress:   s_II =  at  q_II = °

Maximum In-Plane Shear Stress
     Max. (Pos.) Shear Stress:   t =  on  q_s,1 = °
     Max. (Neg.) Shear Stress:      t =  on  q_s,2 = ° 

      Normal Stress on both faces:   s_ave=