Bending Moment Calculator
Free Bending moment Calculator for structural engineering projects. Enter dimensions to get material lists and cost estimates.
Bending Moment Calculator
Calculator
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Formula: M_max = wLยฒ/8 (simply supported, uniform) | M_max = Pab/L (simply supported, point)
Worked example โ Maximum moment = 100 kip-ft, Maximum shear = 20 kips
Formula
M_max = wLยฒ/8 (simply supported, uniform) | M_max = Pab/L (simply supported, point)
The maximum bending moment depends on the load type and support conditions. For a simply supported beam with uniform load w over span L, the maximum moment at midspan is wL-squared divided by 8. For a concentrated load P at distance a from one support, the maximum moment at the load point is P times a times b divided by L, where b equals L minus a.
Worked Examples
Example 1: Simply Supported Beam with Uniform Load
Problem:A 20-foot simply supported beam carries a uniform load of 2 kips per foot. Find the maximum bending moment and shear.
Solution:M_max = wLยฒ/8 = 2 * 20ยฒ / 8 = 100 kip-ft V_max = wL/2 = 2 * 20 / 2 = 20 kips Total load = 2 * 20 = 40 kips
Result:Maximum moment = 100 kip-ft, Maximum shear = 20 kips
Example 2: Cantilever with Point Load
Problem:A 10-foot cantilever beam has a 5-kip point load at the free end.
Solution:M_max = P * L = 5 * 10 = 50 kip-ft (at fixed support) V_max = P = 5 kips
Result:Maximum moment = 50 kip-ft at the fixed end
Frequently Asked Questions
What is a bending moment and why is it important?
A bending moment is the internal moment at any section of a beam caused by external loads and reactions. It represents the tendency of the beam to bend or flex at that point. The magnitude of the bending moment directly determines the bending stresses in the beam, which must remain below the material yield strength. Engineers use bending moment diagrams to identify the critical section where the moment is maximum and design the beam accordingly.
How do support conditions affect the maximum bending moment?
Support conditions have a dramatic effect on bending moments. A simply supported beam with uniform load has a maximum moment of wL-squared over 8 at midspan. A fixed-fixed beam with the same load has a moment of wL-squared over 12 at the supports and wL-squared over 24 at midspan, reducing the peak moment by 33 percent. A cantilever beam has wL-squared over 2 at the fixed end, which is four times larger than the simply supported case. Choosing proper support conditions is a key design decision.
What is the difference between a point load and a uniform load?
A point load (or concentrated load) is a single force applied at one specific location on the beam, like a column bearing on a girder. A uniform load is distributed evenly along the entire length, like the self-weight of a concrete slab or a floor load. Point loads create sharp peaks in the shear diagram and kinks in the moment diagram, while uniform loads create linear shear and parabolic moment curves. Most real beams carry a combination of both load types.
How do I convert bending moment to bending stress?
Bending stress is calculated from the bending moment using the flexure formula: sigma = M * c / I, where M is the bending moment, c is the distance from the neutral axis to the extreme fiber, and I is the moment of inertia of the cross section. For a rectangular section, this simplifies to sigma = 6M / (b * d-squared). The bending stress must be less than the allowable stress for the beam material, which is typically 0.6 times the yield stress for steel per AISC ASD.
What are shear and moment diagrams and how are they related?
They plot internal shear force and bending moment along the length of the member. The two are linked by calculus: shear at any section is the slope of the moment diagram, and the change in moment between two sections equals the area under the shear diagram between them. That relationship gives a fast check, since the moment must peak wherever shear passes through zero and must close to zero at a free or simply supported end.
How does unbraced length affect the moment a steel beam can actually carry?
A beam only develops its full cross-section moment capacity if the compression flange is braced against sideways movement. As the unbraced length between brace points grows, the member can fail by lateral-torsional buckling, twisting and displacing laterally at a moment well below the section capacity the bending stress check implies. Short bracing spacings allow the plastic moment; longer ones give progressively lower capacity. Decking or joists fixed to the compression flange usually supply that bracing.
When should I use an influence line rather than a single fixed load case?
An influence line plots how one response, such as the moment at a chosen section or a support reaction, varies as a unit load travels across the span. Use it whenever the load position is not fixed: crane runway girders, bridge axle groups, or beams carrying relocatable equipment. You then place the moving loads at the ordinates that maximise the response instead of guessing a critical position. For fixed dead and floor live loads one load case suffices.
What is the difference between sagging and hogging moments?
A sagging or positive moment bows the member downward, putting the bottom fibres in tension and the top in compression, which is the pattern at midspan of a simply supported beam. A hogging or negative moment does the reverse over a support in a continuous beam or at the fixed end of a cantilever. The distinction determines where flexural reinforcement is placed in concrete and which flange needs bracing in steel.
What is the section modulus and how do I use it to size a member?
Section modulus S equals the moment of inertia divided by the distance from the neutral axis to the extreme fibre, so bending stress is simply the moment divided by S. To size a member, divide the design moment by the allowable or design bending stress to get the required S, then choose a shape whose tabulated value exceeds it. Convert foot-pounds of moment to inch-pounds before dividing by S in cubic inches.
Why is the moment zero at a simple support but not at a fixed one?
A pin or roller allows the beam end to rotate freely, and a support that cannot resist rotation cannot deliver a moment, so the diagram closes to zero there. A fixed support clamps that rotation, and the restraining action appears as an end moment. Real connections fall between these idealisations, which is why semi-rigid connections are sometimes modelled with a rotational spring rather than either extreme.
References
Background & Theory
History
Reviewed for accuracy by Abdullah, Technical Content Specialist ยท Editorial policy
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