Free Beam Calculator — SFD, BMD, Deflection & Reactions

Beam analysis is the backbone of structural engineering. Every building, bridge, and industrial structure relies on beams to carry loads across openings and transfer forces to columns and foundations.

This page covers the theory, formulas, and worked examples for the most common beam configurations. Use the links below to jump straight to a calculator:

Types of Beams by Support Condition

Simply Supported Beam

A beam with a pin support at one end and a roller at the other. The most common configuration in building construction.

Cantilever Beam

A beam fixed at one end and free at the other.

Fixed-Fixed (Built-In) Beam

A beam rigidly connected at both ends. Reduces midspan moment and deflection compared to simply supported.

Propped Cantilever

A cantilever with an additional simple support at the free end. One degree of indeterminacy.

Continuous Beam

A beam spanning over three or more supports. Statically indeterminate.

Load Types

Point Load (Concentrated Load)

A single force applied at a specific location along the beam.

Simply supported beam, point load P at midspan:

Uniformly Distributed Load (UDL)

A constant load per unit length (w) applied across the full span.

Simply supported beam, UDL w:

Partial UDL

A UDL applied over only a portion of the span. Requires integration or superposition.

Triangular Load

A linearly varying load, common in hydrostatic pressure and snow drift.

Simply supported, triangular load (0 to w₀):

Moment Applied at Support

An external moment applied at a support point. Common in moment frames.

Simply Supported Beam Formulas Table

Load Case Max Moment Max Shear Max Deflection Location
Point load P at midspan PL/4 P/2 PL³/(48EI) Midspan
Point load P at distance a Pab/L Pa/L (if a < b) Pab(L+b)√(3a(L+b))/(27LEI)¹ At load point
UDL w wL²/8 wL/2 5wL⁴/(384EI) Midspan
Triangular 0 to w₀ w₀L²/12√3 w₀L/4 w₀L⁴/(120EI) Varies
Two equal point loads at 1/3 pts PL/3 P 23PL³/(648EI) Midspan

¹ Simplified for a ≤ b. The exact formula involves the position.

Cantilever Beam Formulas Table

Load Case Max Moment Max Shear Max Deflection
Point load P at free end PL P PL³/(3EI)
UDL w across full length wL²/2 wL wL⁴/(8EI)
Triangular 0 (free) to w₀ (fixed) w₀L²/6 w₀L/2 w₀L⁴/(30EI)
Moment M at free end M 0 ML²/(2EI)

Fixed-Fixed Beam Formulas Table

Load Case Moment at Support Moment at Midspan Max Deflection
Point load P at midspan PL/8 PL/8 PL³/(192EI)
UDL w wL²/12 wL²/24 wL⁴/(384EI)

Note: Fixed-fixed deflection for UDL is exactly 1/5 of simply supported deflection. This is why rigid connections reduce floor vibration.

Worked Example: Simply Supported W18x55 Under UDL

Given:

Step 1: Reactions RA = RB = wL/2 = 1.5 × 30/2 = 22.5 kips

Step 2: Maximum Moment Mmax = wL²/8 = 1.5 × 30²/8 = 168.75 kip-ft

Step 3: Bending Stress Check (LRFD) φMn = φFySx = 0.9 × 50 × 98.3 / 12 = 368.6 kip-ft Mu = 168.75 kip-ft < φMn = 368.6 kip-ft ✓

Step 4: Deflection (Service Load) Service w = 1.0 kip/ft (unfactored) Δmax = 5wL⁴/(384EI) = 5 × 1.0/12 × 360⁴ / (384 × 29000 × 890) = 5 × 0.0833 × 16,796,160,000 / 9,908,224,000 = 0.707 in

L/360 = 360/360 = 1.0 in Δmax = 0.707 in < 1.0 in ✓ (passes L/360 deflection limit)

Shear Force and Bending Moment Diagrams

The SFD and BMD are graphical representations of the internal forces in a beam:

Key relationships:

Reading SFD/BMD:

Beam Design Checklist

When designing a steel beam, verify all of the following:

  1. Flexure (strong axis): Mu ≤ φMn where φMn = φFyZx (compact, LRFD)
  2. Shear: Vu ≤ φVn where φVn = 0.6φFyAw (web shear)
  3. Lateral-Torsional Buckling (LTB): Check if Lb ≤ Lp (compact), Lp < Lb ≤ Lr (inelastic), or Lb > Lr (elastic)
  4. Deflection: Δmax ≤ L/360 (floors), L/240 (roofs), L/180 (wind)
  5. Web crippling: Check concentrated loads per AISC Chapter J
  6. Serviceability: Vibration, floor frequency, occupant comfort
  7. Connection capacity: Verify end connections can deliver the assumed support conditions

Use the beam capacity calculator for automated checks per AISC 360, AS 4100, EN 1993, or CSA S16.

Beam Analysis Methods Comparison

Method Type Accuracy Best For
Equilibrium (statics) Hand calc Exact Determinate beams, simple cases
Three-moment equation Hand calc Exact Continuous beams, 2-3 spans
Moment distribution (Hardy Cross) Hand calc Exact Continuous beams, non-prismatic
Slope-deflection Hand calc Exact Frames with sway
Matrix stiffness (FEA) Computer Exact Complex structures, many spans
Portal method Approximate ±10-20% Preliminary frame design
Cantilever method Approximate ±10-20% Tall frames

For day-to-day beam design, the simple beam calculator handles equilibrium-based analysis instantly. For continuous beams, use the continuous beam tool.

Frequently Asked Questions

What is the difference between SFD and BMD? The Shear Force Diagram shows internal shear V(x) along the beam. The Bending Moment Diagram shows internal moment M(x). They are related: dM/dx = V.

How do I calculate beam reactions? For a simply supported beam, sum vertical forces (ΣFy = 0) and moments about one support (ΣM = 0). This gives two equations for two unknowns.

What is the maximum deflection of a simply supported beam with UDL? Δmax = 5wL⁴/(384EI). This occurs at midspan. For L/360 deflection limit, set this equal to L/360 and solve for the required I.

What is the strongest beam shape? For a given weight, the I-beam (W-shape) is the strongest in bending because material is concentrated at the flanges far from the neutral axis, maximizing Ix and Sx.

How do I account for lateral-torsional buckling? If the compression flange is not braced, the beam may buckle laterally before reaching its full plastic moment. Check LTB per AISC Chapter F using the beam capacity calculator.

What is the difference between elastic and plastic analysis? Elastic analysis keeps all stresses below Fy (uses Sx). Plastic analysis allows stress redistribution up to the plastic moment Mp = FyZx (uses Zx). LRFD uses plastic analysis for compact sections.

When should I use a continuous beam vs simply supported? Continuous beams reduce midspan moment and deflection. Use them when you have multiple spans and can detail rigid connections. Simply supported is simpler and more tolerant of foundation settlement.

Can I use these calculators for wood or concrete beams? The beam analysis (SFD, BMD, deflection) works for any material. But code-specific capacity checks are for steel per AISC 360, AS 4100, EN 1993, and CSA S16 only.

Related Pages

Beam Selection Guide by Application

Residential Floor Beams

Typical spans: 10-25 ft. Typical loads: 40-50 psf live + 10-15 psf dead.

Span (ft) Load (klf) Recommended Shape Ix (in⁴) Weight (lb/ft)
10 0.5 W8x31 110 31
15 0.6 W12x26 204 26
20 0.8 W14x48 484 48
25 1.0 W18x55 890 55
30 1.2 W21x68 1,530 68

Roof Purlins

Typical spans: 15-30 ft. Typical loads: 20-30 psf snow + 10-15 psf dead. Often governed by deflection.

Crane Runway Beams

Governed by fatigue, deflection (L/800 or stricter), and lateral loads from crane. Must check web crippling, local flange bending, and lateral-torsional buckling simultaneously.

Deflection Limits Summary

Application Limit Typical Code Reference
Floor beams (live load) L/360 IBC Table 1604.3
Floor beams (total load) L/240 IBC Table 1604.3
Roof beams (live load) L/360 IBC Table 1604.3
Roof beams (total load) L/180 IBC Table 1604.3
Crane runway beams L/800 AISC DG7
Prestressed/masonry Per design ACI 318, TMS 402
Pedestrian vibration L/360 + freq check AISC DG11

The deflection calculator at /tools/beam-deflection/ checks all common limits automatically.

Connection Types and Their Effect on Beam Analysis

The assumed support condition directly affects the moment diagram and deflection:

Simple Shear Connection (Web Angle, Single Plate, End Plate)

Moment Connection (Fully Welded, Bolted End Plate, Extended End Plate)

Partially Restrained Connection

Always verify that your analysis assumptions match the actual connection detail. A beam modeled as simply supported but with stiff end plates will develop unintended negative moments at the supports.

Frequently Asked Questions (Extended)

How do I calculate beam reactions for multiple point loads? Use superposition. Calculate the reaction from each load separately, then sum. For a simply supported beam: RA = Σ(Pi × bi/L) where bi is the distance from load i to support B.

What is the difference between a beam and a girder? No technical difference. In practice, "girder" typically refers to a larger beam that supports other beams. Both are analyzed the same way.

How do I handle a beam with a notch or coped end? A cope reduces the section properties at the connection. Check the remaining web for shear, block shear, and local buckling. The coped section may govern the beam capacity. See coped beam reference.

What is beam camber? Camber is an upward curvature built into a beam at fabrication to offset anticipated dead load deflection. Typically 75-80% of calculated dead load deflection. Does not affect live load deflection checks.

How do I analyze a beam with a varying cross-section? Divide into segments with constant properties. Apply equilibrium on each segment with compatible boundary conditions. Alternatively, use the continuous beam tool with segment properties.

What about shear deformation in short beams? For span-to-depth ratio L/d < 10, shear deformation becomes significant. The Euler-Bernoulli beam theory (which neglects shear) overestimates stiffness. Timoshenko beam theory accounts for this.

How do concentrated loads near supports affect the beam? Concentrated loads near supports primarily stress the web in shear and crippling. Check web crippling per AISC Chapter J10. The moment diagram shows a steep gradient near the load point.

What is the effective length of a cantilever beam for LTB? For a cantilever with free end, Lb = the cantilever length. The LTB check uses the full cantilever length with appropriate Cb factors. Bracing the top flange at mid-span significantly improves LTB capacity.

How do I account for beam self-weight in calculations? Add the beam weight per foot (from AISC Table 1-1) to the dead load. For a W18x55, add 55 lb/ft = 0.055 kips/ft to the distributed load. This is typically small but should be included in deflection checks.

Disclaimer

This is a calculation tool, not a substitute for professional engineering certification. All results must be independently verified by a licensed Professional Engineer (PE) or Structural Engineer (SE) before use in construction, fabrication, or permit documents. The user is responsible for the accuracy of all inputs and the verification of all outputs.