Beam Deflection Calculator

Choose a beam and load case, enter inputs with units, and calculate the maximum deflection.

Mode (beam & load)
Inputs
Tip: steel ≈ 200 GPa, concrete ≈ 25–35 GPa.
Unit changes preserve the same physical quantity and recalculate from the stored source value.
Results
Maximum deflection δmax
Select a case and calculate to see the governing formula.
Location of δmax
Measured from the left support or fixed end.
Step-by-step derivation
Enter values and click Calculate to see the formula, SI substitutions, and result.
References
  • Euler–Bernoulli beam theory for small deflections: deflection varies inversely with E·I.
  • Standard closed-form max-deflection cases are used for simply supported and cantilever beams.
  • The off-center simply supported point-load case evaluates the valid stationary point to get the true maximum deflection.
Actions

A beam can remain below its material-strength limit yet bend enough to damage finishes, affect drainage, cause misalignment, or create uncomfortable movement. The Beam Deflection Calculator estimates maximum elastic deflection for common simply supported and cantilever beam arrangements using span, load, material stiffness, and section stiffness.

What the Beam Deflection Calculator Calculates

The Beam Deflection Calculator supports six idealized beam and load cases:

  • Simply supported beam with a point load at midspan
  • Simply supported beam with a uniform distributed load
  • Simply supported beam with an off-center point load
  • Cantilever beam with a point load at the free end
  • Cantilever beam with a uniform distributed load
  • Cantilever beam with an applied end moment

The calculator reports the estimated maximum deflection and its location measured from the left support or fixed end. It also converts the selected inputs into compatible units and shows the formula and substitutions.

Beam Deflection Inputs

  • L — span length: Distance between supports or from the fixed end to the free end.
  • E — Young’s modulus: The material’s elastic modulus.
  • I — area moment of inertia: The section’s resistance to bending about the loaded axis.
  • P — point load: A concentrated transverse load.
  • w — uniform load: Load applied per unit length across the beam.
  • M — end moment: A moment applied at the cantilever’s free end.
  • a — load position: Distance from the left support to an off-center point load.

Use properties that correspond to the actual material, cross-section, bending axis, support condition, and load case. A moment of inertia about the wrong axis can produce a substantially incorrect result.

How to Use the Beam Deflection Calculator

  1. Select the beam support and load case that matches the intended model.
  2. Enter the clear span or cantilever length.
  3. Enter Young’s modulus for the material and condition being analyzed.
  4. Enter the area moment of inertia about the correct bending axis.
  5. Enter the required point load, distributed load, end moment, or load position.
  6. Check every selected unit carefully.
  7. Click Calculate.
  8. Review the maximum deflection, its location, and the derivation.

Include beam self-weight in the distributed load when it is relevant. The calculator does not automatically know the beam’s material density, cross-sectional area, or self-weight.

Beam support and load-case diagrams showing simply supported and cantilever beams under point loads, uniform loads, an off-center load, and an end moment
Common simply supported and cantilever beam cases used when estimating maximum deflection.

Beam Deflection Formulas

The following equations are standard small-deflection, elastic beam relationships for idealized supports and loads.

Simply Supported Beam With Center Point Load

δmax = PL3 ÷ (48EI)

Maximum deflection occurs at midspan.

Simply Supported Beam With Uniform Load

δmax = 5wL4 ÷ (384EI)

Maximum deflection occurs at midspan when the load is uniform across the complete span.

Cantilever With End Point Load

δmax = PL3 ÷ (3EI)

Maximum deflection occurs at the free end.

Cantilever With Uniform Load

δmax = wL4 ÷ (8EI)

Maximum deflection occurs at the free end.

Cantilever With End Moment

δmax = ML2 ÷ (2EI)

Maximum deflection occurs at the free end.

For an off-center point load on a simply supported beam, the position of maximum deflection is not necessarily the load position or midspan. The Beam Deflection Calculator evaluates the valid stationary point on the deflection curve and reports its location.

Why EI and Span Length Matter

The product EI represents flexural rigidity:

Flexural rigidity = Young’s modulus × area moment of inertia

Increasing either E or I reduces the predicted deflection. Increasing the span can increase deflection dramatically:

  • Point-load deflection commonly varies with L3.
  • Uniform-load deflection commonly varies with L4.

This means a modest span increase can create a much larger deflection even when the load and section remain unchanged.

Worked Beam Deflection Example

Consider a simply supported beam with:

  • Span L = 3.5 m
  • Midspan point load P = 25 kN
  • Young’s modulus E = 200 GPa
  • Area moment of inertia I = 8,000 cm4

Convert the inputs to compatible SI units:

  • P = 25,000 N
  • E = 200,000,000,000 Pa
  • I = 0.00008 m4

Apply the midspan point-load formula:

δmax = (25,000 × 3.53) ÷ (48 × 200,000,000,000 × 0.00008)

δmax ≈ 0.001396 m = 1.40 mm

The estimated maximum elastic deflection is approximately 1.40 mm at midspan.

How to Interpret the Result

Maximum deflection describes the largest displacement predicted by the selected elastic model. It does not automatically determine whether that displacement is acceptable.

Allowable deflection depends on factors such as:

  • Applicable building or engineering code
  • Beam material and structural system
  • Dead, live, wind, snow, equipment, and other load combinations
  • Supported finishes, glazing, partitions, ceilings, or machinery
  • Drainage and ponding requirements
  • Vibration and occupant comfort
  • Short-term versus long-term response

Do not assume a generic span ratio such as L/240 or L/360 applies to every beam. The required limit and load combination must come from the relevant code, specification, manufacturer, or qualified structural engineer.

Assumptions and Limitations

The formulas assume:

  • Linear-elastic material behavior
  • Small deflection relative to the span
  • A straight, prismatic beam with constant E and I
  • Idealized pin, roller, or fixed supports
  • Static loading in one bending plane
  • Bending deformation governed by Euler–Bernoulli beam theory
  • No significant shear deformation

The calculator does not directly account for:

  • Material yielding or failure
  • Cracking or tension stiffening in reinforced concrete
  • Concrete creep, shrinkage, or long-term deflection
  • Composite action unless reflected in the entered EI
  • Connection, bearing, or support flexibility
  • Beam buckling, lateral-torsional buckling, or local buckling
  • Vibration, impact, fatigue, temperature, settlement, or dynamic loading
  • Multiple loads or complex load combinations

For reinforced concrete, timber, composite, tapered, deep, cracked, or non-prismatic members, a simple constant-EI formula may not represent actual behavior adequately.

Common Input Mistakes

  • Entering GPa as though it were Pa
  • Confusing cm4, mm4, in4, and m4
  • Entering total distributed load instead of load per unit length
  • Measuring cantilever length from the wrong point
  • Using the weak-axis I value when bending occurs about the strong axis, or vice versa
  • Leaving out beam self-weight or another relevant service load
  • Selecting a simply supported case for a beam with significant connection restraint

For related introductory mechanics calculations, see the Work and Power Calculator or the Pressure Calculator.

Structural Safety Note

A small calculated deflection does not prove that a beam, connection, support, floor, roof, platform, or structure is safe. Structural design also requires appropriate loads, strength checks, stability checks, serviceability limits, connection design, material factors, and compliance with the governing code.

For buildings, bridges, occupied structures, lifting equipment, platforms, retaining systems, or other safety-critical work, calculations should be reviewed by a qualified structural engineer.

Frequently Asked Questions

What does a Beam Deflection Calculator determine?

It estimates the maximum elastic displacement and its location for the selected idealized beam, support, and load case.

What is EI in beam deflection?

EI is flexural rigidity. E represents material stiffness, while I represents the cross-section’s geometric resistance to bending about the selected axis.

Why does beam deflection increase so quickly with span?

Common point-load formulas contain L3, while uniform-load formulas contain L4. Deflection therefore increases rapidly as span length increases.

Does the calculator check whether a beam is strong enough?

No. Beam strength, shear, bending stress, buckling, connections, and design-code compliance require separate checks.

Can the Beam Deflection Calculator be used for final structural design?

The Beam Deflection Calculator is suitable for educational and preliminary estimates. Safety-critical or final structural design requires complete code-based analysis by a qualified professional.

Sources

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