Analyze center loaded beams with confidence. See stress, deflection, inertia, and section modulus instantly today. Export results, compare examples, and inspect response curves visually.
| Case | Shape | Load | Span | Section Input | Young’s Modulus | Stress | Deflection |
|---|---|---|---|---|---|---|---|
| Example 1 | Rectangular | 500 N | 300 mm | 20 mm × 10 mm | 69 GPa | 56.25 MPa | 2.4457 mm |
| Example 2 | Circular | 1000 N | 400 mm | Diameter 20 mm | 200 GPa | 127.324 MPa | 0.8488 mm |
| Example 3 | Custom | 1500 N | 600 mm | Z = 5000 mm³, I = 60000 mm⁴ | 210 GPa | 45 MPa | 0.5357 mm |
For a simply supported beam with a single load at midspan, the maximum bending moment is:
M = PL / 4
The bending stress at the outer surface is:
σ = M / Z
The midspan deflection is:
δ = PL³ / (48EI)
For a rectangular section:
I = bd³ / 12 and Z = bd² / 6
σ = 3PL / (2bd²)
For a circular section:
I = πd⁴ / 64 and Z = πd³ / 32
σ = 8PL / (πd³)
Each support reaction equals P / 2. Outer fiber strain is σ / E. Factor of safety is Yield Strength / Bending Stress.
It represents the highest bending stress at the outer surface of a beam loaded at midspan between two supports. It helps estimate whether the beam remains below allowable stress.
Use it when the beam cross section is a rectangle and the entered width and depth describe the loaded orientation correctly. Depth strongly affects the result because it is squared or cubed in beam formulas.
Longer spans increase bending moment directly and deflection even faster. In a center loaded beam, stress grows with span, while deflection grows with the cube of span.
Yes. It calculates midspan deflection using the elastic beam equation with the entered load, span, Young’s modulus, and second moment of area.
Yes, if the material behaves close to linear elastic in the tested range and you know its modulus and strength. For strongly nonlinear materials, results become approximate.
It is the ratio of yield strength to calculated bending stress. Values above one indicate the elastic stress is below yield, while larger values indicate more margin.
Custom input lets you use nonstandard beam shapes when you already know section modulus and second moment of area from design tables, CAD, or hand calculations.
No. These equations assume elastic beam theory. Once yielding, cracking, or large deformation begins, actual stress distribution and deflection can differ from the calculator result.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.