Beam Deflection Calculator
Interactive beam deflection simulator with live shear force and bending moment diagrams. Drag loads and supports to see instant deflection curves. Includes cantilever and simply supported beam presets.
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Loading simulation, please waitBeam Deflection Calculator: Interactive Tool for Engineers
✓ Verified Content: All equations, formulas, and reference data in this simulation have been verified by the Simulations4All engineering team against authoritative sources including NIST, peer-reviewed publications, and standard engineering references. See verification log
Any structural engineer will tell you: a beam that deflects too much is a failed beam, even if it never breaks. Sagging floors feel unsafe to occupants, cracked plaster signals problems to building owners, and doors that jam indicate structural distress. In 1978, the Hartford Civic Center roof collapsed under snow load, not from overstress, but from excessive deflection that triggered progressive buckling of the space frame.
The load has to go somewhere, and when loads travel through a beam, they create internal shear forces and bending moments that force the beam to curve. This interactive beam deflection calculator lets you explore exactly how different loads, support conditions, and material properties combine to determine whether your beam stays flat enough to function or sags into failure. Experienced designers know that deflection limits, not strength, often govern beam sizing in modern construction.
How to Use This Simulation
This interactive beam analysis tool computes deflection curves, shear force diagrams, and bending moment diagrams in real time as you modify loads and beam properties. Any structural engineer will tell you that understanding how these three diagrams relate is fundamental to safe beam design.
Main Controls
| Control | Location | Function |
|---|---|---|
| Support Type | Top button row | Choose simply-supported, cantilever, or fixed-fixed boundary conditions |
| Load Type | Second button row | Select point load, uniformly distributed load (UDL), or triangular load |
| Material Preset | Dropdown menu | Quick-select material properties for steel, aluminum, timber, and more |
| Section Calculator | Collapsible panel | Compute moment of inertia from cross-section dimensions |
Input Parameters
| Parameter | Range | Units | What It Controls |
|---|---|---|---|
| Load P (point) | 1-100 | kN | Magnitude of concentrated force |
| Load w (distributed) | 1-50 | kN/m | Intensity of UDL or triangular load |
| Load Position | 10-90 | % span | Location of point load along beam |
| Elastic Modulus E | 1-300 | GPa | Material stiffness (higher = less deflection) |
| Moment of Inertia I | 1-1000 | ×10⁶ mm⁴ | Section geometry resistance to bending |
| Beam Length L | 1-20 | m | Total span between supports |
Results Display
The simulation presents three synchronized diagrams:
- Beam Visualization: Shows the applied loads, support conditions, and reaction forces. This is where structures fail when reactions aren't properly considered.
- Shear Force Diagram (SFD): Displays how transverse forces vary along the beam. Jumps occur at point loads; slopes occur under distributed loads.
- Bending Moment Diagram (BMD): Shows the internal moment distribution. Maximum moment locations are where bending stresses peak.
- Deflection Curve: The final deformed shape with maximum deflection labeled in mm.
Key values displayed in the results panel:
- Support reactions Ra and Rb (kN)
- Maximum shear force Vmax (kN)
- Maximum bending moment Mmax (kN·m)
- Maximum deflection δmax (mm)
Tips for Exploration
-
Watch the L³ effect. Double the span length and observe that deflection increases by a factor of 8 (2³). The load has to go somewhere, and on a longer beam, that somewhere includes much more vertical sag. This cubic relationship is why span is the dominant factor in deflection calculations.
-
Compare support conditions. Under the same load, a fixed-fixed beam deflects about 5× less than a simply-supported beam. This is where structures fail: when designers assume rigid connections that actually behave as pins, real deflections far exceed calculated values.
-
Explore the section calculator. Start with a solid rectangle and see how moment of inertia scales with height cubed (I = bh³/12). Then switch to an I-beam and notice how moving material to the flanges achieves similar stiffness with far less weight. Any structural engineer will tell you that this efficiency is why steel sections are shaped the way they are.
-
Move the point load. Slide a point load from one end to the other and watch the moment diagram change shape. Maximum moment occurs when the load is at midspan for simply-supported beams, but at the fixed end for cantilevers.
-
Try the deflection quiz. Use the interactive quiz to test your intuition. If you can predict how deflection changes when you double the load or halve the modulus, you understand the governing equation δ ∝ PL³/EI.
How to Calculate Beam Deflection: Step-by-Step Tutorial
Follow this guide to calculate beam deflection using our interactive tool or by hand:
Step 1: Identify Your Beam Type
- Simply Supported: Pin at one end, roller at other (most common)
- Cantilever: Fixed at one end, free at other (balconies, diving boards)
- Fixed-Fixed: Both ends restrained (continuous construction)
Step 2: Determine the Loading
- Point load P (kN) - concentrated force at a specific location
- Distributed load w (kN/m) - spread over beam length
- Load position a - distance from left support
Step 3: Gather Material Properties
- Elastic Modulus E (GPa) - material stiffness (Steel: 200, Aluminum: 69)
- Moment of Inertia I (mm⁴) - cross-section property from tables
Step 4: Apply the Beam Deflection Formula
Use the appropriate beam deflection equation from the reference table below.
Step 5: Check Against Code Limits
Compare your calculated deflection to allowable limits (typically L/360 for floors).
Cantilever vs Simply Supported Beam: Deflection Comparison
Understanding the difference between cantilever beam deflection and simply supported beam deflection is critical for design:
| Property | Simply Supported Beam | Cantilever Beam |
|---|---|---|
| Support Conditions | Pin + Roller at ends | Fixed at one end only |
| Deflection Formula (Point Load) | δ = PL³/(48EI) at center | δ = PL³/(3EI) at free end |
| Relative Stiffness | 16× stiffer than cantilever | Very flexible |
| Max Moment Location | At point of load (see SFD/BMD diagrams) | At fixed support |
| Typical Applications | Floor beams, bridge spans | Balconies, canopies, signs |
| Practical Span Range | 6-15 m typical | 1-4 m typical |
Key Insight: A cantilever deflects 16× more than a simply supported beam of the same span under the same load! This is why cantilever spans are kept short.
Beam Deflection Formulas: Complete Reference Guide
Use these standard beam deflection equations for common loading cases:
Simply Supported Beam Deflection Formulas
| Loading Case | Maximum Deflection | Location |
|---|---|---|
| Central Point Load P | δmax = PL³/(48EI) | At midspan (L/2) |
| Point Load at distance a | δmax = Pa²(L-a)²/(3EIL) at load | Under load |
| Uniform Distributed Load w | δmax = 5wL⁴/(384EI) | At midspan (L/2) |
| Triangular Load (zero at ends) | δmax = wL⁴/(120EI) | At 0.519L from lighter end |
Cantilever Beam Deflection Formulas
| Loading Case | Maximum Deflection | Location |
|---|---|---|
| End Point Load P | δmax = PL³/(3EI) | At free end |
| Point Load at distance a | δmax = Pa²(3L-a)/(6EI) | At free end |
| Uniform Distributed Load w | δmax = wL⁴/(8EI) | At free end |
| Moment M at free end | δmax = ML²/(2EI) | At free end |
Fixed-Fixed Beam Deflection Formulas
| Loading Case | Maximum Deflection | Location |
|---|---|---|
| Central Point Load P | δmax = PL³/(192EI) | At midspan |
| Uniform Distributed Load w | δmax = wL⁴/(384EI) | At midspan |
Understanding Moment of Inertia for Beams
The moment of inertia (I) is crucial for beam deflection calculations. Higher I means less deflection.
| Cross-Section | Moment of Inertia Formula | Typical Use |
|---|---|---|
| Rectangle (bh) | I = bh³/12 | Timber beams |
| Circle (diameter d) | I = πd⁴/64 | Solid shafts |
| Hollow Circle | I = π(D⁴-d⁴)/64 | Pipes, tubes |
| I-Beam (W-section) | Use steel tables (AISC) | Steel construction |
Design Tip: Doubling the depth of a rectangular beam increases I by 8× (since I ∝ h³), but only doubles the weight. This is why deep beams are efficient!
Maximum Beam Deflection: Design Limits and Safety Factors
Building codes specify maximum beam deflection limits to ensure:
- Serviceability (floors feel solid, not bouncy)
- Prevent damage to attached elements (windows, partitions)
- Aesthetic requirements (visible sag is unacceptable)
- Equipment function (crane rails must stay aligned)
Code Deflection Limits (IBC, AISC, ACI)
| Application | Limit (Live Load) | Limit (Total Load) | Why |
|---|---|---|---|
| Floor Beams | L/360 | L/240 | Prevent ceiling cracks, occupant comfort |
| Roof Beams (no ceiling) | L/180 | L/120 | Less stringent - no attached elements |
| Roof Beams (with ceiling) | L/240 | L/180 | Protect ceiling from cracking |
| Supporting Glass | L/175 | - | Prevent glass breakage |
| Supporting Masonry | L/600 | L/480 | Masonry is brittle |
| Cantilevers | L/180 | L/120 | Visible deflection |
| Crane Rails | L/600-L/1000 | - | Precision alignment |
Safety Factor Considerations
- Load Factors: Live load × 1.6, Dead load × 1.2 (LRFD method)
- Long-term Effects: Add 50-100% for creep in concrete/wood
- Dynamic Loads: Impact factor 1.25-2.0 for moving loads
- Temperature: Consider thermal expansion in restrained beams
Learning Objectives
After mastering this beam deflection calculator, you will be able to:
- Calculate deflection for simply supported and cantilever beams
- Compare deflection between different beam types and loadings
- Understand why deflection scales with L³ (critical for span design)
- Apply code deflection limits (L/360, L/240, etc.)
- Interpret shear force and bending moment diagrams
- Select appropriate beam sections using moment of inertia
Exploration Activities
Activity 1: Compare Cantilever vs Simply Supported
- Select "Simply Supported", set P = 50 kN at center, L = 10 m
- Note the deflection (should be ~10-15 mm for typical steel beam)
- Switch to "Cantilever" with same load at free end
- Deflection jumps to ~160-200 mm — that is 16× more!
- Takeaway: Cantilevers need much stiffer sections or shorter spans
Activity 2: The L³ Effect
- Set L = 5 m, note the deflection value
- Double L to 10 m — deflection increases by 8× (2³ = 8)
- This is why span is the most sensitive parameter!
- Reducing span is often more effective than increasing beam size
Activity 3: EI Optimization
- Set E = 200 GPa (steel), I = 100 × 10⁶ mm⁴
- Try doubling E to 400 GPa — deflection halves
- Return E to 200, double I to 200 × 10⁶ — deflection also halves
- Insight: Increasing I (deeper section) is usually cheaper than changing material
Activity 4: Code Compliance Check
- Set L = 8 m, calculate L/360 = 22.2 mm (floor limit)
- Adjust E and I until deflection is below 22.2 mm
- This is real structural design — iterating until code is satisfied
Real-World Applications
- Building Floors: Steel W-beams designed to L/360 for occupant comfort and partition protection
- Bridge Girders: Plate girders with L/800 limits to prevent excessive vibration under traffic
- Parking Structures: Post-tensioned concrete beams with camber to counteract long-term creep
- Aircraft Wings: Aluminum cantilever spars with controlled deflection for aerodynamic stability
- Crane Runways: Heavy steel sections with L/600+ limits for trolley wheel alignment
- Residential Decks: Timber joists sized for bounce-free walking (natural frequency > 8 Hz)
Material Properties for Beam Design
| Material | E (GPa) | Density (kg/m³) | Typical I-beam depth (m span) |
|---|---|---|---|
| Structural Steel (A992) | 200 | 7850 | L/20 to L/24 |
| Aluminum 6061-T6 | 69 | 2700 | L/15 to L/18 |
| Reinforced Concrete | 25-35 | 2400 | L/12 to L/16 |
| Glulam Timber | 12-14 | 500 | L/15 to L/20 |
| GFRP Composite | 40 | 1800 | L/15 to L/18 |
Challenge Questions
- Calculation: A simply supported beam has L = 6 m, P = 20 kN at center, E = 200 GPa, I = 50 × 10⁶ mm⁴. Calculate the maximum deflection. Is it within L/360?
- Comparison: For the same load and span, rank these from smallest to largest deflection: simply supported, cantilever, fixed-fixed.
- Design: A 10 m floor beam must not deflect more than L/360 = 27.8 mm under 30 kN/m. What minimum I is needed if E = 200 GPa?
- Analysis: Why does a cantilever beam at a building corner need to be much stiffer than an interior simply supported beam?
- Critical Thinking: If you can only halve the deflection by changing one parameter (E, I, L, or P), which would you choose in practice and why?
Common Mistakes to Avoid
Any structural engineer will tell you that these errors show up repeatedly in student work and even professional calculations:
- Wrong formula: Using cantilever formula for simply supported beam (16x error!). This is where structures fail when designers grab the wrong equation from the table.
- Unit errors: Mixing mm and m in calculations (most common mistake). In the real world, nothing catches this error until the beam sags visibly.
- Ignoring L³: Underestimating how sensitive deflection is to span length. Doubling the span increases deflection 8×, not 2×.
- Strength vs Stiffness: A beam can be strong enough but deflect too much. Experienced designers check both criteria.
- Forgetting long-term: Concrete creep can double deflection over 5 years. What looks fine at first sags unacceptably over time.
- Wrong I value: Using Iy instead of Ix for vertical bending. The load has to go somewhere, and using the wrong I sends your calculations in the wrong direction.
Key Formulas Summary
Flexural Rigidity:
EI = E × I (N·m² or kN·m²)
Moment-Curvature Relationship:
M = EI × (d²y/dx²)
Typical I Values (Standard Steel Sections):
| Section | Ix (×10⁶ mm⁴) |
|---|---|
| W200×36 | 34.4 |
| W310×60 | 128 |
| W410×85 | 316 |
| W530×109 | 666 |
Frequently Asked Questions
What is beam deflection and why does it matter?
Beam deflection is the vertical displacement of a beam under load. It matters because excessive deflection causes cracked finishes, jammed doors, bouncy floors, and occupant discomfort—even when the beam is strong enough to carry the load. Building codes limit deflection to L/360 for floors and L/240 for roofs to prevent these serviceability problems [1].
What is the beam deflection formula for a simply supported beam?
For a simply supported beam with a central point load P, the maximum deflection formula is δmax = PL³/(48EI), occurring at midspan. For a uniformly distributed load w, use δmax = 5wL⁴/(384EI). These formulas assume linear elastic behavior and small deflections [2].
How do I calculate moment of inertia for beam sections?
Moment of inertia (I) depends on cross-section shape. For a solid rectangle: I = bh³/12 where b is width and h is height. For a circle: I = πd⁴/64. For standard steel sections like W-shapes, use AISC steel tables. Deeper sections have dramatically higher I values because I scales with height cubed [3].
What deflection limit should I use for floor beams?
The most common limit is L/360 for live load deflection on floor beams per IBC and AISC specifications. For total load (dead + live), use L/240. More stringent limits apply when supporting brittle materials: L/480 for plaster ceilings, L/600 for masonry walls. Crane rails may require L/600 to L/1000 for precision alignment [4].
Why does a cantilever deflect more than a simply supported beam?
A cantilever with end load deflects 16 times more than a simply supported beam with the same central load and span. This is because the cantilever formula is δ = PL³/(3EI) compared to δ = PL³/(48EI) for simply supported. The ratio is 48/3 = 16. This is why cantilever spans are kept much shorter in practice [2].
How does beam length affect deflection?
Deflection is proportional to L³ (length cubed) for point loads and L⁴ for distributed loads. Doubling the span increases deflection by a factor of 8 for point loads. This cubic relationship makes span the most sensitive parameter in beam design—reducing span is often more effective than increasing beam size [1].
Verification Log
| Claim/Data | Source | Status | Date Verified |
|---|---|---|---|
| Simply supported center load formula: δ = PL³/48EI | AISC Steel Manual, MIT OCW 2.002 | ✓ Verified | Dec 2025 |
| Cantilever end load formula: δ = PL³/3EI | Roark's Formulas for Stress & Strain | ✓ Verified | Dec 2025 |
| Fixed-fixed center load formula: δ = PL³/192EI | Timoshenko Strength of Materials | ✓ Verified | Dec 2025 |
| Steel E = 200 GPa typical value | AISC, Engineering Toolbox | ✓ Verified | Dec 2025 |
| Deflection limits L/360, L/240 | IBC, AISC Design Guide | ✓ Verified | Dec 2025 |
| Standard section Ix values | AISC Shapes Database | ✓ Verified | Dec 2025 |
| Superposition principle for beam analysis | Hibbeler Mechanics of Materials | ✓ Verified | Dec 2025 |
Written by Simulations4All Team
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