Bending Stress Calculator
Calculate maximum bending stress in beams using sigma = My/I.
Calculator
From neutral axis to outer fiber
Results
Max Bending Stress
0.13MPa
198019.80mm^3
Visualizations
Results Overview
Formula
Bending stress equals bending moment times distance from neutral axis divided by moment of inertia.
Alternative Form
Variables
| Symbol | Name | Unit | Description |
|---|---|---|---|
| sigma | Bending Stress | MPa | Maximum normal stress at extreme fiber |
| M | Bending Moment | N*m | Internal bending moment at the section |
| y | Distance to Fiber | mm | Distance from neutral axis to extreme fiber |
| I | Moment of Inertia | mm^4 | Area moment of inertia about bending axis |
| S | Section Modulus | mm^3 | S = I/y, geometric measure of bending strength |
Explanation
Bending stress varies linearly across the section. Maximum stress at the fiber farthest from the neutral axis.
Derivation
From Euler-Bernoulli beam theory: epsilon = -y/r. With Hooke law sigma = E*epsilon gives sigma = My/I.
Step-by-Step Calculation
Follow each step to understand how the result is calculated from your inputs.
Determine the bending moment M at the critical section
Calculate moment of inertia I for the cross-section
Find distance y from neutral axis to extreme fiber
Calculate sigma = My/I
Compare against allowable stress with safety factor
Worked Examples
See how the calculator works with different scenarios.
Scenario
A W200x22 steel I-beam (I = 20.0E6 mm^4, c = 101 mm) carries M = 25 kN*m.
Inputs
Calculation
sigma = 25000*1000*101/20000000 = 126.3 MPa.
Result
sigma = 126.3 MPa
Interpretation
Within yield strength of structural steel (250 MPa). Safety factor ~2.0.
Understanding Your Result
Your Result: Max Bending Stress: 0.13 MPa
Typical range: Steel: 100-200 MPa. Wood: 5-12 MPa. Aluminum: 50-150 MPa.
What This Means
Bending stress is the normal stress resisting bending deformation. One face in tension, the opposite in compression.
Why It Matters
Exceeding yield causes permanent deformation; exceeding ultimate causes fracture.
Professional Interpretation
Compare against allowable stress (yield/safety factor). Verify deflection limits.
Recommendations
- •Use I-beams or hollow sections for efficiency
- •Check both strength and deflection
- •Apply stress concentrations at notches
Educational Content
Introduction
Bending is one of the most common loading conditions in structural and mechanical engineering.
Concept Explanation
sigma = My/I assumes plane sections remain plane (Euler-Bernoulli theory). Stress varies linearly from neutral axis.
Applications
Benefits
- •Simple and widely validated formula
- •Applicable to any symmetric cross-section
- •Foundation for complex analyses
Limitations
- •Valid only for elastic range
- •Does not account for shear lag
- •Not valid for very short or deep beams
Best Practices
- •Calculate I accurately
- •Use correct y to extreme fiber
- •Include stress concentrations
Common Misconceptions
Practical Tips
- •I-beams are most efficient for bending
- •Deep sections reduce stress but increase deflection
- •Check stress at maximum moment points
- •For asymmetric sections check both tensile and compressive stresses
Common Mistakes
Assumptions
This calculator makes the following assumptions to provide estimates:
Limitations
Be aware of these limitations when using this calculator:
Frequently Asked Questions
Answers to common questions about this calculator.
What is bending stress?
What is the bending stress formula?
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Glossary
Technical terms used in mortgage calculations explained in plain language.
- Bending Stress
- Normal stress due to bending moment: sigma = My/I.
- Neutral Axis
- Line where bending stress is zero.
- Section Modulus
- S = I/y_max, geometric measure of bending strength.
- Moment of Inertia
- I = integral(y^2 dA), resistance to bending deflection.
Authoritative References
Trusted sources and standards referenced by this calculator.
Applicable Standards
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Page Information
2025-08-21
2.0.0
Free to use for educational and professional purposes.