# A Visual Guide to Mohr's Circle for Plane Stress Analysis

> Explore stress transformation in materials with our FREE online Mohr’s Circle calculator and interactive 2D stress visualizer.

Source: https://unboreng.com/blog/mohr-circle-guide-and-interactive-visualizer-app/
Published: May 11, 2025

> Try Mohr Circle Visualizer (free): https://unboreng.com/apps/mohr-circle/

Imagine a tiny, almost invisible square element within a structural beam, a machine component, or even the ground beneath us. This element is constantly subjected to internal forces – pulls, pushes, and sliding actions. We collectively call this internal resistance to external forces **stress**. Understanding stress is fundamental in engineering mechanics and stress analysis.

In many 2D (**plane stress**) scenarios, we start by knowing the stresses acting on the faces of this element aligned with our standard x and y axes:
-   Normal stress $\sigma_x$ (perpendicular to the x-face)
-   Normal stress $\sigma_y$ (perpendicular to the y-face)
-   Shear stress $\tau_{xy}$ (parallel to the x-face, in the y-direction, and its counterpart $\tau_{yx}$ on the y-face)

  *[Diagram: 2D Plane Stress Element Diagram]*
  *Fig 1: A 2D stress element showing normal stresses and shear stresses. Tensile normal stresses $\sigma_x, \sigma_y$ are positive. The shear stress $\tau_{xy}$ (input value) is positive if it causes clockwise rotation on the +x face. Consequently, $\tau_{yx} (= -\tau_{xy})$ causes counter-clockwise rotation on the +y face.*

But what if we need to know the **stresses on a plane** *tilted* at an angle $\theta$ relative to our x-axis? Let the new axes aligned with this tilted plane be x' and y'. The normal stress on the x'-face is denoted $\sigma_{x'}$ (or sometimes $\sigma_n$), and the shear stress on the x'-face acting in the y'-direction is $\tau_{x'y'}$ (or sometimes $\tau_{nt}$). These stresses will generally be different from $\sigma_x$ and $\tau_{xy}$. This is the core of **stress transformation**.
When plotting on Mohr's Circle, the point representing the stress state on the x'-face (Point X') has coordinates $(\sigma_{x'}, -\tau_{x'y'})$.

To calculate these transformed stresses, engineers use the following **stress transformation equations**:

$$ \sigma_{x'} = \frac{\sigma_x + \sigma_y}{2} + \frac{\sigma_x - \sigma_y}{2} \cos(2\theta) + \tau_{xy} \sin(2\theta) $$

$$ \sigma_{y'} = \frac{\sigma_x + \sigma_y}{2} - \frac{\sigma_x - \sigma_y}{2} \cos(2\theta) - \tau_{xy} \sin(2\theta) $$

$$ \tau_{x'y'} = -\left(\frac{\sigma_x - \sigma_y}{2}\right) \sin(2\theta) + \tau_{xy} \cos(2\theta) $$

Although these equations provide exact solutions, their complexity can make it challenging to develop an intuitive understanding of stress transformation. Fortunately, Mohr's Circle offers a brilliant graphical method that greatly simplifies **plane stress analysis**!

## Mohr's Circle: Simplifying Stress Transformation

In the late 19th century, German engineer Christian Otto Mohr developed a graphical technique called **Mohr's Circle**. It elegantly visualizes the **state of stress** at a point and allows us to determine stresses on any plane, including **principal stresses** and **maximum shear stress**, by simple geometry.

## Constructing Mohr's Circle: A Step-by-Step Guide for Stress Analysis

Let's build Mohr's Circle for a given state of plane stress $(\sigma_x, \sigma_y, \tau_{xy})$.

**1. Establish the Coordinate System for Mohr's Circle:**
   - The horizontal axis represents **Normal Stress ($\sigma$)**. Positive $\sigma$ (tensile) is to the right; negative $\sigma$ (compressive) is to the left.
   - The vertical axis represents **Shear Stress ($\tau$)**. This sign convention is crucial:
     - Shear stress on an element face that tends to cause **Counter-Clockwise (CCW) rotation** of the element is plotted **above** the $\sigma$-axis (positive $\tau$).
     - Shear stress that tends to cause **Clockwise (CW) rotation** is plotted **below** the $\sigma$-axis (negative $\tau$).

  *[Diagram: Mohr's Circle Coordinate Axes for Normal and Shear Stress]*
  *Fig 2: Coordinate system for Mohr's Circle, defining positive normal stress (σ) and shear stress (τ) conventions.*

**2. Plot Two Key Points (X and Y):**
   We represent the stress state on the original x and y faces as two points on this $\sigma-\tau$ plane:
   -   **Point X:** Represents the stress state on the face whose outward normal is the x-axis. Its coordinates are $(\sigma_x, -\tau_{xy})$. The $-\tau_{xy}$ is because if the input $\tau_{xy}$ is positive (defined as causing CW rotation on the x-face as in Fig 1), it's plotted in the negative $\tau$ region of the circle.
   -   **Point Y:** Represents the stress state on the face whose outward normal is the y-axis. Its coordinates are $(\sigma_y, \tau_{xy})$. If input $\tau_{xy}$ is positive (CW on x-face), then $\tau_{yx} = -\tau_{xy}$ causes CCW rotation on the y-face, so it's plotted in the positive $\tau$ region.

**3. Locate the Center of Mohr's Circle (C):**
   The center of Mohr's Circle always lies on the $\sigma$-axis. It represents the **average normal stress**:
   $$ C = \sigma_{avg} = \frac{\sigma_x + \sigma_y}{2} $$
   The coordinates of the center are $(C, 0)$.

**4. Determine the Radius of Mohr's Circle (R):**
   The line segment connecting Point X and Point Y is a diameter of the circle. The radius can be found using the distance from the center C to either Point X or Point Y:

   $$ R = \sqrt{\left( \frac{\sigma_x - \sigma_y}{2} \right)^2 + \tau_{xy}^2} $$

**5. Draw Mohr's Circle:**
   Using the center $(C, 0)$ and the calculated radius $R$, draw the circle.

  *[Diagram: Example Construction of Mohr's Circle for a Given Stress State]*
  *Fig 3: Constructing Mohr's Circle for stress transformation. Example: $\sigma_x=60, \sigma_y=-20, \tau_{xy}=30$ (input, implies CW shear on x-face). Point X is (60,-30), Y is (-20,30). Center C is (20,0), Radius R is 50.*

## Interpreting Mohr's Circle: Finding Principal Stresses and Max Shear

This single circle is packed with critical information for stress analysis:

-   **Any Point on the Circumference:** Each point $(\sigma, \tau)$ on the circle's edge represents the **normal stress** and **shear stress** on a particular plane through the material.
-   **Angles on the Circle vs. Reality:** A physical rotation of a plane by an angle $\theta$ (say, counter-clockwise) from the original x-face corresponds to a rotation of **$2\theta$** (two-theta) on Mohr's Circle, **in the same direction** (CCW), starting from the line CX (Center to Point X).
-   **Principal Stresses ($\sigma_1, \sigma_2$):** These are the maximum and minimum normal stresses at the point. They occur where the circle intersects the $\sigma$-axis (i.e., where shear stress $\tau = 0$). These are crucial for predicting material failure.
    -   Maximum Principal Stress: $\sigma_1 = C + R$
    -   Minimum Principal Stress: $\sigma_2 = C - R$
    
    The planes on which these stresses act are called **principal planes**.
-   **Maximum Shear Stress ($\tau_{max}$):** The highest and lowest points on the circle give the **maximum in-plane shear stress**.
    -   Magnitude: $|\tau_{max}| = R$
    -   On the planes of maximum shear, the normal stress is $\sigma_{avg} = C$.

  *[Diagram: Interpreting Key Features of Mohr's Circle]*
  *Fig 4: Key features from Mohr's Circle: Principal stresses ($\sigma_1, \sigma_2$), maximum shear stress ($\tau_{max}$), and the $2\theta$ angle relationship to find transformed stresses $(\sigma',\tau')$ on an arbitrary plane.*

## The Power of Visualization in Stress Analysis with Mohr's Circle

Mohr's Circle is an invaluable tool in engineering mechanics because it:
1.  **Builds Intuition:** It provides a clear visual understanding of how **normal and shear stresses** change with the orientation of the plane.
2.  **Identifies Critical Values:** It instantly highlights the most important stresses for design and failure analysis: **principal stresses** $\sigma_1, \sigma_2$, and **maximum shear stress** $\tau_{max}$. Materials often yield or fracture when these stresses reach their material strength limits.
3.  **Simplifies Calculations:** Once drawn, it allows for quick graphical determination of stresses on any plane, bypassing repeated use of complex **stress transformation equations**.

## Explore Mohr's Circle Interactively for Plane Stress!

Reading about Mohr's Circle is a great start, but seeing it respond to changes in real-time truly solidifies understanding. I've developed an interactive web application where you can:
-   Input your own values for plane stresses $\sigma_x, \sigma_y$, and $\tau_{xy}$.
-   Set an angle $\theta$ for the plane of interest.
-   Instantly see Mohr's Circle drawn, along with the rotated stress element and all calculated values including **principal stresses** and **transformed stresses**.

Experiment with different stress states and rotation angles to see how the circle and the stresses on the element change. It's a fantastic way to learn stress analysis!

Give it a try and master the art of **stress transformation** with Mohr's Circle! If you have any questions or feedback, feel free to reach out.

For beams, the normal and shear stresses you transform here come from the internal bending moment and shear force. See how to draw those in our guide to [shear and moment diagrams](/blog/shear-force-bending-moment-diagram/).