Mohr's circle

Mohr's circle, named after Christian Otto Mohr, is a two-dimensional graphical representation of the state of stress at a point. The abscissa, \sigma_\mathrm{n}\,\!, and ordinate, \tau_\mathrm{n}\,\!, of each point on the circle are the normal stress and shear stress components, respectively, acting on a particular cut plane with a unit vector \mathbf n\,\! with components \left(n_1, n_2, n_3 \right)\,\!. In other words, the circumference of the circle is the locus of points that represent the state of stress on individual planes at all their orientations.

Karl Culmann was the first to conceive a graphical representation for stresses while considering longitudinal and vertical stresses in horizontal beams during bending. Mohr's contribution extended the use of this representation for both two- and three-dimensional stresses and developed a failure criterion based on the stress circle.[1]

Other graphical methods for the representation of the stress state at a point include the Lame's stress ellipsoid and Cauchy's stress quadric.

Contents

Mohr's circle for two-dimensional stress states

A two-dimensional Mohr's circle can be constructed if we know the normal stresses \sigma_x, \sigma_y, and the shear stress \tau_{xy}. The following sign conventions are usually used:

  1. Tensile stresses (positive) are to the right.
  2. Compressive stresses (negative) are to the left.
  3. Clockwise shear stresses are plotted upward.
  4. Counterclockwise shear stresses are plotted downward.

The reason for the above sign convention is that, in engineering mechanics[2], the normal stresses are positive if they are outward to the plane of action (tension), and shear stresses are positive if they rotate clockwise about the point in consideration. In geomechanics, i.e. soil mechanics and rock mechanics, however, normal stresses are considered positive when they are inward to the plane of action (compression), and shear stresses are positive if they rotate counterclockwise about the point in consideration.[1][3][4][5]

To construct the Mohr circle of stress for a state of plane stress, or plane strain, first we plot two points in the \sigma_\mathrm{n}:\tau_\mathrm{n}\,\! space corresponding to the known stress components on both perpendicular planes, i.e. A(\sigma_y, \tau_{xy})\,\! and B(\sigma_x, -\tau_{xy})\,\! (Figure 1 and 2). We then connect points A\,\! and B\,\! by a straight line and find the midpoint O\,\! which corresponds to the intersection of this line with the \sigma_\mathrm{n}\,\! axis. Finally, we draw a circle with diameter \overline{AB}\,\! and centre at O\,\!.

The radius R\,\! of the circle is R = \sqrt{\left[\tfrac{1}{2}(\sigma_x - \sigma_y)\right]^2 %2B \tau_{xy}^2}\,\!, and the coordinates of its centre are \left[\tfrac{1}{2}(\sigma_x %2B \sigma_y), 0\right]\,\!.

The principal stresses are then the abscissa of the points of intersection of the circle with the \sigma_\mathrm{n}\,\! axis (note that the shear stresses are zero for the principal stresses).

Drawing a Mohr's circle

The following procedure is used to draw a Mohr's circle and to find the magnitude and direction of maximum stresses from it.

\sigma_\text{avg}=\tfrac{1}{2}(\sigma_x%2B \sigma_y).

\sigma_1 = \sigma_\max = \tfrac{1}{2}(\sigma_x %2B \sigma_y) %2B \sqrt{\left[\tfrac{1}{2}(\sigma_x- \sigma_y)\right]^2%2B \tau_{xy}^2}

\sigma_2 = \sigma_\min = \tfrac{1}{2}(\sigma_x %2B \sigma_y) - \sqrt{\left[\tfrac{1}{2}(\sigma_x- \sigma_y)\right]^2%2B \tau_{xy}^2}

\tau_{\max,\min}= \pm \sqrt{\left[\tfrac{1}{2}(\sigma_x- \sigma_y)\right]^2%2B {\tau_{xy}}^2}
.
\phi = 2\theta_{p1} = \arctan\left[2\tau_{xy}/(\sigma_x- \sigma_y)\right].
2\theta_s =  \arctan\left[-(\sigma_x - \sigma_y)/(2\tau_{xy})\right]. It is important to pay attention to the use of these two equations as they look similar.

The previous discussion assumes, implicitly, that there are two orthogonal directions x and y that define a plane in which the stress components \sigma_x\,\!. \sigma_y\,\!, and \tau_{xy}\,\! are known. It is also implicit that these stresses are known at a point P\,\! in a continuum body under plane stress or plane strain. The Mohr circle, once drawn, can be used to find the components of the stress tensor for any other choice of orthogonal directions in the plane.

Stress components on an arbitrary plane

Using the Mohr circle one can find the stress components (\sigma_\mathrm{n}, \tau_\mathrm{n})\,\! on any other plane with a different orientation \theta\,\! that passes through point P\,\!. For this, two approaches can be used:

Mohr's circle for a general three-dimensional state of stresses

To construct the Mohr's circle for a general three-dimensional case of stresses at a point, the values of the principal stresses \left(\sigma_1, \sigma_2, \sigma_3 \right)\,\! and their principal directions \left(n_1, n_2, n_3 \right)\,\! must be first evaluated.

Considering the principal axes as the coordinate system, instead of the general x_1\,\!, x_2\,\!, x_3\,\! coordinate system, and assuming that \sigma_1 > \sigma_2 > \sigma_3\,\!, then the normal and shear components of the stress vector \mathbf T^{(\mathbf n)}\,\!, for a given plane with unit vector \mathbf n\,\!, satisfy the following equations

\begin{align}
\left( T^{(n)} \right)^2 &= \sigma_{ij}\sigma_{ik}n_jn_k \\
\sigma_\mathrm{n}^2 %2B \tau_\mathrm{n}^2 &= \sigma_1^2 n_1^2 %2B \sigma_2^2 n_2^2 %2B \sigma_3^2 n_3^2 \end{align}\,\!
\sigma_\mathrm{n} = \sigma_1 n_1^2 %2B \sigma_2 n_2^2 %2B \sigma_3 n_3^2\,\!

Knowing that n_i n_i = n_1^2%2Bn_2^2%2Bn_3^2 = 1\,\!, we can solve for n_1^2\,\!, n_2^2\,\!, n_3^2\,\!, using the Gauss elimination method which yields

\begin{align}
n_1^2 &= \frac{\tau_\mathrm{n}^2%2B(\sigma_\mathrm{n} - \sigma_2)(\sigma_\mathrm{n} - \sigma_3)}{(\sigma_1 - \sigma_2)(\sigma_1 - \sigma_3)} \ge 0\\
n_2^2 &= \frac{\tau_\mathrm{n}^2%2B(\sigma_\mathrm{n} - \sigma_3)(\sigma_\mathrm{n} - \sigma_1)}{(\sigma_2 - \sigma_3)(\sigma_2 - \sigma_1)} \ge 0\\
n_3^2 &= \frac{\tau_\mathrm{n}^2%2B(\sigma_\mathrm{n} - \sigma_1)(\sigma_\mathrm{n} - \sigma_2)}{(\sigma_3 - \sigma_1)(\sigma_3 - \sigma_2)} \ge 0
\end{align}\,\!

Since \sigma_1 > \sigma_2 > \sigma_3\,\!, and (n_i)^2\,\! is non-negative, the numerators from the these equations satisfy

\tau_\mathrm{n}^2%2B(\sigma_\mathrm{n} - \sigma_2)(\sigma_\mathrm{n} - \sigma_3) \ge 0\,\! as the denominator \sigma_1 - \sigma_2 > 0\,\! and \sigma_1 - \sigma_3 > 0\,\!
\tau_\mathrm{n}^2%2B(\sigma_\mathrm{n} - \sigma_3)(\sigma_\mathrm{n} - \sigma_1) \le 0\,\! as the denominator \sigma_2 - \sigma_3 > 0\,\! and \sigma_2 - \sigma_1 < 0\,\!
\tau_\mathrm{n}^2%2B(\sigma_\mathrm{n} - \sigma_1)(\sigma_\mathrm{n} - \sigma_2) \ge 0\,\! as the denominator \sigma_3 - \sigma_1 < 0\,\! and \sigma_3 - \sigma_2 < 0\,\!

These expressions can be rewritten as

\begin{align}
\tau_\mathrm{n}^2 %2B \left[ \sigma_\mathrm{n}- \tfrac{1}{2} (\sigma_2 %2B \sigma_3) \right]^2 \ge \left( \tfrac{1}{2}(\sigma_2 - \sigma_3) \right)^2 \\
\tau_\mathrm{n}^2 %2B \left[ \sigma_\mathrm{n}- \tfrac{1}{2} (\sigma_1 %2B \sigma_3) \right]^2 \le \left( \tfrac{1}{2}(\sigma_1 - \sigma_3) \right)^2 \\
\tau_\mathrm{n}^2 %2B \left[ \sigma_\mathrm{n}- \tfrac{1}{2} (\sigma_1 %2B \sigma_2) \right]^2 \ge \left( \tfrac{1}{2}(\sigma_1 - \sigma_2) \right)^2 \\
\end{align}\,\!

which are the equations of the three Mohr's circles for stress C_1\,\!, C_2\,\! , and C_3\,\!, with radii R_1=\tfrac{1}{2}(\sigma_2 - \sigma_3)\,\!, R_2=\tfrac{1}{2}(\sigma_1 - \sigma_3)\,\! , and R_3=\tfrac{1}{2}(\sigma_1 - \sigma_2)\,\!, and their centres with coordinates \left[\tfrac{1}{2}(\sigma_2 %2B \sigma_3), 0\right]\,\!, \left[\tfrac{1}{2}(\sigma_1 %2B \sigma_3), 0\right]\,\!, \left[\tfrac{1}{2}(\sigma_1 %2B \sigma_2), 0\right]\,\!, respectively.

These equations for the Mohr's circles show that all admissible stress points (\sigma_\mathrm{n}, \tau_\mathrm{n})\,\! lie on these circles or within the shaded area enclosed by them (see Figure 3). Stress points (\sigma_\mathrm{n}, \tau_\mathrm{n})\,\! satisfying the equation for circle C_1\,\! lie on, or outside circle C_1\,\!. Stress points (\sigma_\mathrm{n}, \tau_\mathrm{n})\,\! satisfying the equation for circle C_2\,\! lie on, or inside circle C_2\,\!. And finally, stress points (\sigma_\mathrm{n}, \tau_\mathrm{n})\,\! satisfying the equation for circle C_3\,\! lie on, or outside circle C_3\,\!.

References

  1. ^ a b Parry
  2. ^ The sign convention differ in disciplines such as mechanical engineering, structural engineering, and geomechanics. The engineering mechanics sign convention is used in this article.
  3. ^ Jumikis
  4. ^ Holtz
  5. ^ Brady
  6. ^ Megson, T.H.G., Aircraft Structures for Engineering Students, Fourth Edition, 2007, section 1.8

Bibliography

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