Continuous Beam Analysis Back
Structural Calculator

Continuous Beam Analysis Calculator

Multi-span continuous beam analysis via the three-moment equation (Clapeyron). Computes support moments, reactions, bending moment diagram, and deflection in real time for 2–5 span beams.

Parameters
Number of spans
Load pattern
Section & Load
Elastic modulus E
GPa
Second moment I
cm⁴
Load intensity q
kN/m
Span lengths (m)
Results
M_max+ [kN·m]
M_max− [kN·m]
Max Reaction [kN]
Max Deflection [mm]
Bending Moment Diagram (BMD)
Bmd
Deflection Diagram
Defl

For adjacent spans $i$ and $i+1$:

$$M_{i-1}L_i + 2M_i(L_i+L_{i+1}) + M_{i+1}L_{i+1}= -\frac{q_i L_i^3}{4}- \frac{q_{i+1}L_{i+1}^3}{4}$$

(equal EI, uniform distributed loads $q$)

Support reactions (span i):

$$R_{i,L}= \frac{q_i L_i}{2}- \frac{M_{i+1}-M_i}{L_i}, \quad R_{i,R}= \frac{q_i L_i}{2}+ \frac{M_{i+1}-M_i}{L_i}$$

Location of max positive moment: $x^* = R_{i,L}/ q_i$

What is Continuous Beam Analysis?

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What exactly is a "continuous beam," and why can't I just analyze each span separately like a simple beam?
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Great question! A continuous beam is one that has more than two supports, like a bridge deck on multiple piers. The key is that the internal bending moment is transferred over the intermediate supports. This connection makes the beam stiffer and reduces the maximum moment compared to separate simple beams. In this simulator, try setting the "Number of spans" to 3 and see how the bending moment is continuous over the middle supports—you can't get that by analyzing each piece alone.
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Wait, really? So how do we actually solve for those internal moments? The math looks intimidating.
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The secret is the Three-Moment Equation. It's a compatibility condition: the slope of the beam must be the same on either side of a support. For instance, over a middle support, the beam can't have a kink. This gives us an equation linking the moments at three consecutive supports. In the simulator, when you change the "Load pattern," the right side of this equation changes, and the tool solves the resulting system of equations instantly to find all the support moments ($M_i$).
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So the "Elastic modulus E" and "Second moment I" are in the existing theory note, but not in the main equation shown. Why are they parameters if they don't appear?
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Sharp observation! The classic Three-Moment Equation simplifies when $EI$ is constant across all spans—the $EI$ terms cancel out. That's the case in this simulator. We include $E$ and $I$ as parameters because in real CAE, you always define material and geometry. They are crucial for calculating actual stress and deflection. Try changing $E$ and $I$ here; you'll see the support reactions and moments don't change, proving the solution depends only on geometry and load for a prismatic beam.

Physical Model & Key Equations

The fundamental governing equation is the Three-Moment Equation (Clapeyron's Theorem). It enforces slope continuity at the interior support i between two adjacent spans, assuming a constant flexural rigidity $EI$ and a uniformly distributed load.

$$M_{i-1}L_i + 2M_i(L_i+L_{i+1}) + M_{i+1}L_{i+1}= -\frac{q_i L_i^3}{4}- \frac{q_{i+1}L_{i+1}^3}{4}$$

Where:
$M_{i-1}, M_i, M_{i+1}$ = Bending moments at supports (unknowns we solve for).
$L_i, L_{i+1}$ = Lengths of the two adjacent spans.
$q_i, q_{i+1}$ = Intensities of the uniformly distributed loads on each span (use the "Load intensity q" and pattern).
The right-hand side represents the fixed-end moments from the loads.

Once support moments are known, we calculate the Reactions. The reaction at support i has contributions from the spans to its left and right.

$$R_{i}= R_{i,L}+ R_{i,R}= \left( \frac{q_i L_i}{2}- \frac{M_{i}-M_{i-1}}{L_i}\right) + \left( \frac{q_{i+1}L_{i+1}}{2}+ \frac{M_{i+1}-M_{i}}{L_{i+1}} \right)$$

Physical Meaning: The first term in each parenthesis ($qL/2$) is the simple beam reaction. The second term ($\Delta M / L$) is a shear correction caused by the continuity moments. This is why reactions at middle supports are higher—they help carry the load from adjacent spans.

Frequently Asked Questions

Yes, this tool supports real-time calculation. When you change the span length or loading conditions, the support moments, reactions, and deflections are immediately recalculated based on Clapeyron's equation, and the bending moment diagram is also updated automatically.
Currently, this tool only supports uniformly distributed loads. If you need to handle concentrated loads or partial loads, please convert them to equivalent uniformly distributed loads or use another general-purpose structural analysis software. We are considering expanding this functionality in the future.
At the bottom of the input panel, the bending moment diagram and deflection curve for each span are displayed as graphs. The diagrams are updated in real time, and the maximum and minimum values can also be checked numerically. The graphs can be zoomed in and out.
In this tool, you can set the moment of inertia and Young's modulus for each span individually. However, it assumes constant EI within the same span. It can correctly calculate cases where different cross sections are used for different spans.

Real-World Applications

Bridge Design: Multi-span highway and railway bridges are classic continuous beams. Using continuity reduces the depth of the deck required, leading to more economical and slender designs. Engineers use this exact analysis to determine maximum moments and shear forces for reinforcement.

Building Floor Systems: Continuous reinforced concrete beams supporting floor slabs are analyzed this way. The load pattern parameter lets you model different live load arrangements (like alternate spans loaded) to find the most critical bending envelope for design.

Industrial Gantry Cranes: The runway beams for overhead cranes are often continuous over multiple supports. Accurate reaction force calculation is vital for designing the supporting columns and foundations to handle the moving load.

CAE Model Validation: Before trusting complex Finite Element Analysis (FEA) of a structure, engineers create simple beam models. The results from this calculator serve as an exact benchmark to verify that the FEM software's beam elements and boundary conditions are set up correctly.

Common Misunderstandings and Points to Note

When you start using this tool, there are a few common pitfalls. First, are you perhaps assuming that all supports are the same as pin supports? The model in this tool treats internal supports as being free to rotate but restrained in vertical movement, much like rollers. However, actual bridge piers are often rigidly connected to foundations or ground and can deform. Keep in mind that the tool's results are a first approximation assuming "ideal, rigid supports."

Next, when setting parameters, get into the habit of considering the "Second Moment of Area I" and the "Modulus of Elasticity E" together. Their product "EI" is the flexural rigidity, the crucial value that determines deflection. For example, using a section with the same I for steel (E=205 GPa) and concrete (E=30 GPa) results in a deflection difference of about 7 times. If you reduce E by a factor of 10 in the tool, you should see the deflection jump by 10 times. In practice, once you choose a material, understanding the EI is your starting line.

Finally, note that the location of maximum deflection does not coincide with the location of maximum bending moment. For a simply supported beam with a uniformly distributed load, it's at the center, but for a continuous beam, it shifts away from the mid-span. For a two-span beam with a uniform load, the maximum deflection is slightly toward the ends from each span's center. Take a close look at the tool's deflection curve and check where the peak is. In design, you check whether the deflection at this location exceeds regulatory limits.