Analyze beam bending for point, uniform, and custom loading cases. View results instantly with charts. Plan stronger members using clear engineering checks and comparisons.
This calculator uses classic Euler-Bernoulli beam equations for small elastic deflections. Internal calculations convert all values to SI units.
Maximum deflection: δmax = P L3 / 48 E I
Reactions: RL = P b / L, RR = P a / L, where b = L - a.
For x ≤ a: y(x) = P b x (L2 - b2 - x2) / 6 L E I
For x ≥ a: y(x) = P a (L - x) (2 L x - x2 - a2) / 6 L E I
Maximum deflection: δmax = 5 w L4 / 384 E I
Maximum deflection: δmax = P L3 / 3 E I
Maximum deflection: δmax = w L4 / 8 E I
| Beam Case | Span | Load | E | I | Approx. Max Deflection |
|---|---|---|---|---|---|
| Simply supported center point | 4.0 m | 12 kN | 200 GPa | 8,000,000 mm⁴ | 10.00 mm |
| Simply supported offset point at 1.5 m | 4.0 m | 15 kN | 200 GPa | 8,000,000 mm⁴ | 11.50 mm |
| Simply supported full uniform load | 5.0 m | 3.5 kN/m | 200 GPa | 8,000,000 mm⁴ | 17.80 mm |
| Cantilever end point | 2.5 m | 8 kN | 200 GPa | 8,000,000 mm⁴ | 26.04 mm |
| Cantilever full uniform load | 2.5 m | 2.0 kN/m | 200 GPa | 8,000,000 mm⁴ | 6.10 mm |
It estimates beam deflection under common support and load cases. It also reports reactions, stiffness, peak location, slopes, and a serviceability comparison.
It covers simply supported beams with center point, offset point, and uniform loads, plus cantilever beams with end point and full uniform loads.
Yes. Choose the custom inertia mode when you already know the section property from a handbook, design sheet, or manufacturer catalog.
Cantilevers are fixed at one end and free at the other. That condition makes them much more flexible than simply supported beams under similar loading.
It is a serviceability target such as L/240, L/360, or L/480. The calculator compares actual deflection with that limit and flags the result.
It shows the analytical elastic deflection curve for the chosen load case. It is idealized and does not include cracking, yielding, or connection slip.
Yes. Enter the correct Young’s modulus and section inertia for your material and member geometry, and the tool will recalculate the response.
This tool assumes linear elastic behavior, constant cross section, small deflections, and standard beam theory. Use detailed structural analysis for critical design work.
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.