The Mechanical
Engineering Handbook




Principal Stresses and Principal Angles Calculator































How This Is Calculated



$$\sigma_{1,2} = \frac{\sigma_x + \sigma_y}{2} \pm \sqrt{\left(\frac{\sigma_x - \sigma_y}{2}\right)^2 + {\tau_{xy}}^2} $$ $$\tan(2\theta_p) = \frac{2 \tau_{xy}}{\sigma_x - \sigma_y} $$ where:

σ1,2   =   Principal Stresses   (N/m² or Pa)

θp   =   Principal Angles  (°)

σx   =   Normal Stress in x direction   (N/m² or Pa)

σy   =   Normal Stress in y direction   (N/m² or Pa)

τxy   =   Shear Stress in xy direction   (N/m² or Pa)


Assumptions



  • The material is homogeneous, isotropic, and continuous.
  • The material follows Hooke's Law, i.e., the stress-strain relationship is linear.
  • The stress in the thickness direction (out-of-plane stress) is assumed to be zero.
  • Deformations are insufficient such that the original geometry is not altered.


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