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Cantilever Steel Beam Calculator

Free cantilever steel beam calculator — instant deflection, moment, shear & AISC code checks for balconies, canopies, crane arms & overhangs.
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The Cantilever Steel Beam Calculator provides accurate analysis for overhang and projecting beams with free-end conditions. Calculate reactions, maximum moment at support, deflection, shear, and AISC-compliant checks for cantilever steel beams.

Optimized for common cantilever scenarios, including balconies, awnings, decks, and swing sets. Input span, uniform or point loads (including at free end), and section properties — instantly receive support moment, tip deflection, shear diagram, utilization ratios, safety factors, and beam weight.

Supports steel sections with LRFD/ASD methods and clear visual diagrams. Perfect for engineers and DIY users. For full multi-support beam design, visit our Ultimate Steel Beam Calculator.

Cantilever Steel Beam Calculator – Overhang, Deflection & AISC Design

Fixed-Free Beam Analysis • AISC 360 / Eurocode 3 • Deflection • Stress • LTB Checks

A cantilever beam is fixed (clamped) at one end and free at the other. The maximum bending moment occurs at the fixed support, and maximum deflection at the free tip. All stress concentrates at the root — making accurate calculation critical for safety.
 Beam Geometry
m

Distance from fixed wall to free tip

m

0 = pure cantilever. Enables uplift check at anchor.

m

For LTB check. Leave blank to use full span.

◑ Cross-Section Properties
⚠ Material Properties
MPa
MPa

Default: 200,000 MPa (29,000 ksi) for steel

↓ Applied Loads
Include beam self-weight (dead load)
Apply LRFD load factors (1.2D + 1.6L)
 Design Code & Limits
×

1.5–2.0 for swing sets, crane arms; 1.0 for static

Enter your beam parameters in the Inputs tab and click Calculate Beam to see results here.
 Demand / Capacity Ratios
 Detailed Results
Parameter Value Units Limit / Capacity Status
 Step-by-Step Derivation
Need a full structural report?

Share your results or export to PDF for engineering review and building permit submission.

 Beam Diagram
Calculate to generate beam diagram
Shear Force Diagram (SFD)
Bending Moment Diagram (BMD)
Deflection Curve
Run a calculation first to generate shear, moment, and deflection diagrams.
All calculations use Euler-Bernoulli beam theory with linear elastic material behavior. Superposition is applied for combined loads. Formulas are shown with LaTeX rendering for clarity.
∆ Deflection Formulas

Maximum Tip Deflection

\[\delta_{max} = \frac{P L^3}{3 E I}\]

Slope at Free Tip

\[\theta = \frac{P L^2}{2 E I}\]

Deflection at Distance x from Fixed End

\[\delta(x) = \frac{P x^2}{6 E I}(3L - x)\]

Where: P = point load [kN], L = span [m], E = elastic modulus [GPa], I = moment of inertia [m⁴]

Maximum Tip Deflection

\[\delta_{max} = \frac{w L^4}{8 E I}\]

Slope at Free Tip

\[\theta = \frac{w L^3}{6 E I}\]

Deflection at x from Fixed End

\[\delta(x) = \frac{w x^2}{24 E I}(x^2 - 4Lx + 6L^2)\]

Where: w = distributed load intensity [kN/m]

Maximum Tip Deflection

\[\delta_{max} = \frac{M_0 L^2}{2 E I}\]

Slope at Free Tip

\[\theta = \frac{M_0 L}{E I}\]
⚡ Bending Moment & Shear
\[M_{max} = P \cdot L\quad \text{(point load at tip)}\] \[M_{max} = \frac{w L^2}{2}\quad \text{(UDL over full span)}\]

Superposition for Multiple Loads

\[M_{total} = \sum_{i} M_i\]

The principle of superposition allows independent effects to be added.

\[V_{max} = P + w L\quad \text{(point + UDL combined)}\]
 Stress Calculations

Elastic Bending Stress

\[\sigma_b = \frac{M_{max}}{S_x} = \frac{M_{max} \cdot c}{I_x}\]

LRFD Strength Check

\[\text{DCR} = \frac{M_u}{\phi_b M_n} \leq 1.0\] where \(\phi_b = 0.90\) and \(M_n = F_y \cdot Z_x\) (compact section yielding)
\[\tau = \frac{V_{max}}{A_w}\] \[\phi_v V_n = 1.0 \times 0.6 F_y A_w\] where \(A_w = d \cdot t_w\) (web area)
\[\text{UCR} = \frac{M_u}{\phi M_n} + \frac{V_u}{\phi V_n} \leq 1.0\]
▲ Lateral-Torsional Buckling (LTB)

Plastic Limit

\[L_p = 1.76\, r_y \sqrt{\frac{E}{F_y}}\]

Elastic Limit

\[L_r = 1.95\, r_{ts} \frac{E}{0.7 F_y}\sqrt{\frac{J \cdot c}{S_x \cdot h_0} + \sqrt{\left(\frac{J \cdot c}{S_x \cdot h_0}\right)^2 + 6.76\left(\frac{0.7 F_y}{E}\right)^2}}\]

Inelastic LTB (L_p < L_b ≤ L_r)

\[M_n = C_b\left[M_p - \left(M_p - 0.7 F_y S_x\right)\frac{L_b - L_p}{L_r - L_p}\right] \leq M_p\]

Elastic LTB (L_b > L_r)

\[M_n = F_{cr} \cdot S_x \leq M_p\]
 Serviceability
\[\delta_{max} \leq \frac{L}{\Delta_{\text{limit}}}\]
ApplicationTypical Limit
General cantileverL/180
Roof / canopyL/240
Occupied floors / balconiesL/360
Vibration-sensitiveL/480
 Vibration / Natural Frequency
\[f_n = \frac{3.516}{2\pi L^2}\sqrt{\frac{EI}{m}}\] where m = mass per unit length (kg/m) including self-weight and imposed mass.

Guideline: f_n > 4 Hz acceptable for occupied floors (AISC Design Guide 11). f_n > 8 Hz for sensitive equipment.

Accuracy Note: This calculator uses Euler-Bernoulli beam theory for prismatic, linear-elastic members. It is intended for preliminary engineering checks. For final structural design, engage a licensed Professional Engineer (PE/CEng) who will apply site-specific conditions, full load combination analysis, connection detailing, and code requirements applicable to your jurisdiction.
◑ W-Shape / IPE Section Properties Database

Click any row to load section properties into the calculator. Properties shown for strong-axis bending.

Section d (mm) bₑ (mm) A (mm²) Iₓ (mm⁴×10⁶) Sₓ (mm³×10³) Zₓ (mm³×10³) rₖ (mm) W (kg/m)
⚡ Section Optimizer

Finds the lightest W-shape from the database that satisfies all strength, deflection, and LTB checks based on your current input parameters.

 Application Presets

Click any preset to automatically populate typical spans, loads, and factors for that application. You can then customize the values.

 Common Load Reference
ApplicationTypical SpanLive LoadDead LoadDeflection Limit
Residential Balcony1.5–3 m2.4 kN/m² (IBC)1.0–2.0 kN/mL/360
Canopy / Awning1.0–4 m0.5–1.5 kN/m²0.5–1.0 kN/mL/240
Jib Crane (light)2–6 m5–50 kN tip loadBeam self-weightL/300–L/500
Swing Set1.5–2.5 m2–3 kN (DLF 2.0)Beam self-weightL/240
Signboard0.5–2 mWind-drivenSign weightL/150
Mezzanine Edge2–4 m3.6 kN/m²2.0–3.5 kN/mL/360
Cantilever Steel Beam Calculator • Uses Euler-Bernoulli beam theory • AISC 360 / Eurocode 3 compliance checks
⚠️ For preliminary design only. Always engage a licensed Professional Engineer (PE/CEng) for final structural design and building permit submission.

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⚙ Complete Engineering Reference Guide

Cantilever Steel Beam Calculator
Step-by-Step User Guide

Full documentation covering every input, formula, result, and engineering principle behind the calculator — from basic deflection checks to AISC 360 LRFD code compliance.

∑ Euler-Bernoulli Theory ▼ AISC 360 / Eurocode 3 ▲ LTB Checks  Metric & Imperial ⚙ 7 Calculation Modules

What Is a Cantilever Steel Beam?

A cantilever beam is a structural member that is rigidly fixed (clamped) at one end and completely free to deflect at the other end. Unlike a simply supported beam where loads spread between two supports, all bending resistance in a cantilever must come from the single fixed support.

w [kN/m] P [kN] δmax L (Cantilever Span) Fixed Support Free End Mmax R Distributed Load (w) Point Load (P) Deflection Curve Max Moment/Reaction (Fixed End)

Fig. 1 — Cantilever beam anatomy: fixed wall, applied loads, deflection curve, and key structural reactions. Maximum moment and shear always occur at the fixed support.

The key engineering challenge of a cantilever is that 100% of bending moment concentrates at the fixed end — unlike simply supported beams where moment distributes across the span. This makes it uniquely critical to get the calculations right.

Real-World Cantilever Applications

Application Typical Span Primary Load Type Critical Check
Residential balcony1.5 – 3.0 mUDL live load (people)Deflection L/360
Canopy / awning1.0 – 4.0 mSnow + wind UDLDeflection L/240
Jib crane arm2.0 – 8.0 mPoint load at tipBending stress + LTB
Swing set arm1.5 – 2.5 mDynamic point load (DLF 2.0)Deflection + fatigue
Deck / floor overhang1.0 – 2.5 mDead + live UDLDeflection L/360
Signboard bracket0.5 – 2.0 mPoint + wind loadTip rotation
Mezzanine edge beam2.0 – 4.0 mDead + live UDL (high)Bending + vibration

Step-by-Step User Guide

Follow these 7 steps in order to complete a full cantilever beam analysis. Each step maps directly to a section of the calculator.

1
Choose Your Unit System (Metric or Imperial)

Click SI / Metric for kN, m, MPa — or Imperial for kip, ft, ksi — in the top-right header toggle. All inputs and outputs switch instantly. Never mix units — this is the #1 source of calculation errors.

If you are in Bangladesh, India, or most of Asia/Europe, use SI / Metric. US projects typically use Imperial (kips, feet, ksi).
2
Enter Beam Geometry

In the Inputs tab, under Beam Geometry, enter:

  • Cantilever Span (L) — The projection length from the fixed wall face to the free tip. m or ft
  • Back-Span Length (optional) — If the cantilever is part of a longer beam that continues back to another support, enter that back-span length. This enables uplift force calculation at the anchor.
  • Unbraced Length (Lb) — Distance between lateral bracing points along the compression flange. Leave blank to default to the full span. m
Common mistake: Entering the total beam length when only the cantilever overhang is the span. L = the overhang distance only, from wall face to free tip.
3
Select Cross-Section Properties

Choose "Select from Database" to pick a standard W-shape, IPE, or HSS section by designation (e.g. W250x25). All section properties (I, S, Z, ry) auto-populate. Or choose "Enter Custom Properties" to manually type Ix, Sx, Zx, ry for non-standard or built-up sections.

You can also browse the full section database in the Section DB tab and click any row to load it. The Optimize tab will automatically find the lightest passing section for your loads.
4
Set Material Properties

Select a steel grade from the dropdown — yield strength (Fy) and elastic modulus (E) auto-fill from code values. You can override with custom values for special alloy steels.

GradeFy (MPa)Fy (ksi)Fu (MPa)Region
A3625036400USA (structural)
A572 Gr.5034550450USA (most common)
A99234550450USA (W-shapes)
S27527539.9430Europe / Eurocode
S35535551.5510Europe (high strength)
Q34534550470China / Asia
5
Add Applied Loads

Click + Point Load, + Distributed Load, or + End Moment to add load rows. For each load, specify:

  • Load Category — D (Dead), L (Live), W (Wind), S (Snow). This controls LRFD load factors.
  • Magnitude — Force in kN (point) or kN/m (distributed).
  • Position — Distance from the fixed end. 0 = fixed wall; L = free tip.

Toggle Include beam self-weight to automatically add the section's dead load. Toggle Apply LRFD factors to use factored loads for strength design.

Use the Presets tab to auto-fill typical loads for balcony, crane, swing set, etc. — then fine-tune the values.
6
Set Design Code & Deflection Limit

Select your governing code (AISC 360, Eurocode 3, etc.) and deflection limit from the dropdown:

  • L/180 — General cantilevers (most permissive)
  • L/240 — Roofs, canopies (default)
  • L/360 — Occupied floors, balconies (most strict)
  • Custom — Enter any ratio

Set the Dynamic Load Factor (DLF) to 2.0 for swing sets or playground equipment; 1.5 for cranes; 1.0 for static loads.

7
Click "Calculate Beam" and Read Results

Press the orange CALCULATE BEAM button. The calculator switches to the Results tab, showing: green/amber/red pass-fail verdict, demand/capacity ratio bars, a detailed results table, and a step-by-step derivation. Visit Diagrams for interactive shear force, moment, and deflection charts.

If any check fails, click Optimize tab to instantly find the lightest W-section that passes all checks for your current loads.

Input Parameters & Units Reference

Every input field in the calculator, with the accepted unit, valid range, and what it represents physically.

Span L
Cantilever projection length from face of fixed support to free tip.
Metric: 0.1 – 50 m
Imperial: 0.3 – 165 ft
Back-Span
Length of beam behind fixed support to next anchor. 0 = pure cantilever.
≥ 0 m / ft
Unbraced Length Lₛ
Distance between lateral bracing points on compression flange. Governs LTB.
Default = full span L
Moment of Inertia Iₓ
Second moment of area about strong axis. Governs stiffness and deflection.
Metric: mm⁴
Imperial: in⁴
Section Modulus Sₓ
Elastic section modulus = Ix / (d/2). Used for elastic bending stress.
Metric: mm³
Imperial: in³
Plastic Modulus Zₓ
Plastic section modulus. Used for full plastic moment capacity Mₚ.
mm³ / in³ (Z > S always)
Radius of Gyration rₖ
Weak-axis radius of gyration. Critical for LTB slenderness calculation.
mm / in
Yield Strength F₵
Steel yield stress. Material strength limit for all code checks.
Metric: MPa (N/mm²)
Imperial: ksi
Elastic Modulus E
Young's modulus of elasticity for steel. Controls stiffness.
Default: 200,000 MPa
= 29,000 ksi
Point Load P
Concentrated force applied at a single point along the beam.
kN or kip; position in m or ft
Distributed Load w
Load spread over a length. Can be partial (start and end position).
kN/m or kip/ft
Dynamic Load Factor
Multiplier for impact/vibration. Applied to all live loads.
1.0 (static) – 2.0 (swing set)

Unit Conversion Quick Reference

QuantityMetric UnitImperial UnitConversion Factor
Length (span)mft1 m = 3.2808 ft
Length (section)mmin1 mm = 0.03937 in
Point ForcekNkip1 kN = 0.2248 kip
Distributed LoadkN/mkip/ft1 kN/m = 0.0685 kip/ft
Bending MomentkN⋅mkip⋅ft1 kN⋅m = 0.7376 kip⋅ft
Stress / PressureMPaksi1 MPa = 0.14504 ksi
Moment of Inertiamm⁴in⁴1 mm⁴ = 2.403×10⁻⁶ in⁴
Section Modulusmm³in³1 mm³ = 6.102×10⁻⁵ in³
Deflectionmmin1 mm = 0.03937 in

All Calculation Formulas Used — Detailed Explanation

Every formula used in the calculator, derived from Euler-Bernoulli beam theory and AISC 360 LRFD provisions. Formulas are rendered in LaTeX for precision.

Deflection Formulas

Deflection (δ) is the vertical displacement of the beam, maximum at the free tip. The calculator uses superposition to add individual load contributions.

δ.1 — Point Load at Free Tip
\[\delta_{max} = \frac{P L^3}{3 E I}\]
P = Point load kN  |  L = Cantilever span m  |  E = Elastic modulus kN/m²  |  I = Moment of inertia m⁴  |  δmax = result in m (converted to mm in output)
δ.2 — Point Load at Intermediate Position a from Fixed End
\[\delta_{tip} = \frac{P a^2 (3L - a)}{6 E I}\]
a = Distance from fixed end to load position m. When a = L, this simplifies to the tip-load formula above.
δ.3 — Uniformly Distributed Load (UDL) over Full Span
\[\delta_{max} = \frac{w L^4}{8 E I}\]
w = Distributed load intensity kN/m. Note the L⁴ term — doubling the span creates 16× more deflection. This is why span control is critical.
δ.4 — Partial UDL from Position x₁ to x₂
\[\delta_{tip} = \frac{w \left[ x_2^3(4L - x_2) - x_1^3(4L - x_1) \right]}{24 E I}\]
x₁ = load start distance from fixed end  |  x₂ = load end distance. The calculator evaluates x₁=0 to x₂=L for full-span UDL to verify against formula δ.3.
δ.5 — Applied End Moment M₀
\[\delta_{max} = \frac{M_0 L^2}{2 E I}\]
M₀ = Applied moment at position a from fixed end kN⋅m. A moment load at the free tip creates constant curvature and the largest deflection per unit of applied load.
δ.6 — Deflection Profile Along Span (for Charts)
\[\delta(x) = \frac{P x^2 (3L - x)}{6 E I} \quad \text{(point load at tip)}\]
\[\delta(x) = \frac{w x^2 (x^2 - 4Lx + 6L^2)}{24 E I} \quad \text{(UDL)}\]
These are evaluated at 50 equally-spaced positions (0 → L) to draw the deflection curve chart.

Slope / Tip Rotation Formulas

Tip rotation (θ) is the angle of the beam's neutral axis at the free end. Excessive rotation causes visual tilt in balconies, water ponding, and equipment misalignment.

θ — Slope at Free Tip
\[\theta_{tip} = \frac{P L^2}{2 E I} \quad \text{(point load at tip)}\]
\[\theta_{tip} = \frac{w L^3}{6 E I} \quad \text{(UDL over full span)}\]
Result in radians. Converted to degrees in results: θ° = θ × (180/π). Typical serviceability limit: ≤ 0.5° (8.7 mrad).

Bending Moment & Shear Force Formulas

M — Maximum Bending Moment at Fixed Support
\[M_{max} = P \cdot a \quad \text{(point load at position a from fixed end)}\]
\[M_{max} = \frac{w L^2}{2} \quad \text{(UDL over full span)}\]
\[M_{max} = \sum_{i} M_i \quad \text{(superposition of all loads)}\]
Units: kN⋅m or kip⋅ft. The negative sign convention (hogging moment at fixed end) is handled internally. The BMD diagram shows this peak negative moment at x = 0.
V — Maximum Shear Force at Fixed Support
\[V_{max} = P + w \cdot L \quad \text{(combined point load + UDL)}\]
Units: kN or kip. Shear is constant between the free tip and any point load, then steps up at each load position. Maximum is always at the fixed wall.

Stress Calculation Formulas

σ — Elastic Bending Stress (Outer Fibre)
\[\sigma_b = \frac{M_{max}}{S_x} = \frac{M_{max} \cdot c}{I_x}\]
Sx = elastic section modulus mm³  |  c = distance from neutral axis to outer fibre = d/2 for symmetric sections. Result in MPa. Must satisfy σₛ ≤ F₵ for elastic design.
τ — Shear Stress in Web
\[\tau = \frac{V_{max}}{A_w} \qquad A_w = d \cdot t_w\]
A₩ = web shear area = section depth × web thickness mm². Result in MPa. Must satisfy τ ≤ 0.6 F₵.

LRFD Strength Capacity Formulas (AISC 360)

LRFD (Load and Resistance Factor Design) applies partial safety factors to both loads and material resistance, giving a more statistically reliable design than older ASD methods.

Factored Load Combination (LRFD)
\[M_u = 1.2\,M_D + 1.6\,M_L \quad \text{(governing combination for most structures)}\]
M₹ = factored design moment (demand)  |  Mₐ = moment from dead loads  |  Mₗ = moment from live loads. Additional combinations: 1.2D + 1.6S, 0.9D + 1.0W.
Mₙ — Plastic Moment Capacity (Section Yielding)
\[M_p = F_y \cdot Z_x\]
\[\phi_b M_n = 0.90 \times M_p \quad \text{(compact section, no LTB)}\]
Zx = plastic section modulus mm³  |  ϕₛ = 0.90 (resistance factor for bending). This is the maximum possible moment capacity when the full cross-section yields.
DCR — Demand-to-Capacity Ratio (Bending)
\[\text{DCR}_{bending} = \frac{M_u}{\phi_b M_n} \leq 1.0 \quad \Rightarrow \text{PASS}\]
DCR < 0.85: GREEN — comfortable margin  |  0.85 – 1.0: AMBER — acceptable, near limit  |  > 1.0: RED — over-stressed, FAIL.
Shear Capacity (AISC 360 ‑G2)
\[V_n = 0.6\,F_y\,A_w \qquad \phi_v V_n = 1.0 \times V_n\]
\[\text{DCR}_{shear} = \frac{V_u}{\phi_v V_n} \leq 1.0\]
ϕₚ = 1.0 for most W-shapes (compact webs). 0.6 F₵ is the shear yield stress per von Mises criterion. Shear rarely governs for cantilevers unless the span is very short.
ASD Safety Factor (Allowable Stress Method)
\[SF = \frac{F_y}{\sigma_b} \geq 1.67 \quad \text{(ASD — no LRFD factors applied)}\]
Safety factor = 1.67 corresponds to the ASD allowable bending stress Fₛ = 0.6 F₵ = F₵/1.67. This is reported alongside LRFD checks for reference.

Lateral-Torsional Buckling (LTB) Formulas — AISC F2

LTB is a failure mode where the compression flange of the beam buckles sideways and twists. It is especially critical for cantilevers because the top flange is in compression over the full span and is often unbraced.

Plastic Limit — No LTB Reduction Below Lₚ
\[L_p = 1.76\, r_y \sqrt{\frac{E}{F_y}}\]
If Lₛ ≤ Lₚ: section achieves full plastic moment Mₙ. No LTB reduction. rₖ = weak-axis radius of gyration mm.
Inelastic LTB — Lₚ < Lₛ ≤ Lᵣ
\[M_n = C_b \left[ M_p - \left(M_p - 0.7 F_y S_x\right) \frac{L_b - L_p}{L_r - L_p} \right] \leq M_p\]
Linear interpolation between full plastic capacity and 70% of elastic yield. Cₛ = moment gradient modifier (1.0 used conservatively for cantilevers).
Elastic LTB — Lₛ > Lᵣ
\[M_n = F_{cr} \cdot S_x \leq M_p\]
\[F_{cr} = \frac{C_b \pi^2 E}{(L_b / r_y)^2}\]
Elastic buckling stress Fԁᵣ governs. Section capacity drops significantly below Mₙ. In this range, adding lateral bracing (reducing Lₛ) is the most effective design improvement.

Serviceability — Deflection Limit Check

Deflection Serviceability Check
\[\delta_{max} \leq \frac{L}{\Delta_{limit}} \quad \Rightarrow \text{PASS}\]
\[\text{DCR}_{deflection} = \frac{\delta_{max}}{L / \Delta_{limit}} \leq 1.0\]
Example: L = 3.0 m, limit = L/360 ➔ allowable deflection = 3000/360 = 8.33 mm. If δmax = 6.5 mm, DCR = 6.5/8.33 = 78% — PASS.

Natural Frequency (Vibration Check)

First Natural Frequency of Cantilever Beam
\[f_n = \frac{3.516}{2\pi L^2} \sqrt{\frac{EI}{m}}\]
m = mass per unit length kg/m (beam self-weight ÷ g). Result in Hz. Guideline: fₙ > 4 Hz = acceptable for occupied structures (AISC Design Guide 11). fₙ > 8 Hz = required for sensitive equipment mounting.

Back-Span Uplift Force

Uplift at Back-Span Anchor
\[R_{uplift} = \frac{M_{max,\,cantilever}}{L_{backspan}}\]
When the cantilever extends beyond a continuous beam, the loads create an uplift (tension) force at the back anchor. This must be resisted by anchor bolts or hold-down connections. Result in kN.

Understanding Your Results — Complete Interpretation Guide

After clicking CALCULATE BEAM, the Results tab shows every structural check. Here is exactly what each value means and how to interpret the color-coded indicators.

DCR Color System

Green (0 – 85%) — Comfortable margin, beam is well within capacity
Amber (85 – 100%) — Acceptable but approaching limit; consider next size up
Red (> 100%) — Exceeds capacity — FAIL; increase section or reduce loads
Result Unit Formula Used Pass Condition If it Fails
Max Deflection δmax mm wL⁴/(8EI) + superposition δ ≤ L/Δ Use deeper section; shorten span; reduce loads
Max Moment Mmax kN⋅m P·L or wL²/2 M₹ ≤ ϕₛMₙ Increase section modulus Zx; change section
Max Shear Vmax kN P + wL V₹ ≤ ϕₚVₙ Add web stiffener; increase web area A₩
Bending Stress σₛ MPa Mmax / Sx σ ≤ F₵ Increase Sx; use higher-grade steel
Tip Rotation θ degrees PL²/(2EI) θ ≤ 0.5° Increase EI; reduce loads; check ponding risk
Safety Factor SF F₵ / σₛ SF ≥ 1.67 Redesign with higher Zx or larger section
Natural Frequency fₙ Hz 3.516/(2πL²) × √(EI/m) fₙ ≥ 4.0 Hz Increase EI; add mass; provide damping
LTB Mode Lp, Lr comparison Yielding governs Add lateral bracing; reduce Lₛ; use wider flange
Uplift at Anchor kN Mmax / Lbackspan ≤ anchor capacity Increase back-span; add hold-downs; add counterweight

How to Read the Shear Force Diagram (SFD)

The SFD shows internal shear force along the beam length. For a cantilever with a point load at the tip, the SFD is a horizontal line equal to P across the full span, stepping to zero at the free tip. A UDL creates a linearly varying SFD, maximum at the fixed end and zero at the tip.

How to Read the Bending Moment Diagram (BMD)

The BMD shows internal bending moment. For a cantilever, moment is always zero at the free tip and maximum (negative / hogging) at the fixed wall. A point load creates a linear BMD; a UDL creates a parabolic curve.

How to Read the Deflection Curve

The deflection curve shows vertical displacement along the span. The fixed end has zero deflection. The curve increases toward the free tip, reaching δmax. If the curve exceeds the allowable deflection line, the serviceability check fails.

Common Mistakes to Avoid — Microcopy Guide

These are the most frequent errors users make. Each mistake is paired with the correct approach.

✕ Wrong

Entering the total beam length (including back-span) as the cantilever span L.

✓ Correct

L = overhang distance only (wall face to free tip). Enter back-span separately in the Back-Span field.

✕ Wrong

Using the same units in some fields and different units in others (mixing kN with kip, or m with ft).

✓ Correct

Set the unit toggle FIRST before entering any values. The toggle converts all labels but NOT previously typed numbers.

✕ Wrong

Ignoring self-weight. A W610x82 beam adds 0.80 kN/m dead load — significant for long cantilevers.

✓ Correct

Always enable "Include beam self-weight." The calculator auto-calculates it from the section's listed kg/m weight.

✕ Wrong

Setting Dynamic Load Factor = 1.0 for swing sets or playground equipment (static analysis only).

✓ Correct

Use DLF = 2.0 for swing sets; DLF = 1.5 for cranes/hoists; DLF = 1.3 for machinery with moderate vibration.

✕ Wrong

Leaving unbraced length = full span when the top flange is actually braced at mid-span.

✓ Correct

Enter the actual distance between lateral supports as Lₛ. Shorter Lₛ gives higher LTB capacity (less reduction).

✕ Wrong

Selecting L/180 deflection limit for a balcony floor used by people (too lenient — floor will feel bouncy).

✓ Correct

Use L/360 for occupied floors and balconies. L/240 for roofs. L/180 only for general non-critical cantilevers.

✕ Wrong

Entering section modulus Sx when the Plastic Modulus Zx is needed (they look the same unit but Zx is always larger).

✓ Correct

For LRFD: use Zx (plastic modulus). For elastic/ASD stress checks: use Sx. Both are listed in the Section DB tab.

✕ Wrong

Classifying all loads as "Dead" to get lower LRFD factors (1.2D instead of 1.6L) — underestimates demand.

✓ Correct

Use correct categories: permanent structure weight = D; people, furniture, equipment = L; snow = S; lateral pressure = W.

Input Validation Rules & Accepted Ranges

The calculator validates all inputs before computing. Here are the accepted ranges and what triggers a warning or error.

Input Field Min Value Max Value Warning Trigger Error Condition
Span L0.1 m50 mL > 10 m (long cantilever warning)L ≤ 0 (no calculation)
Unbraced Length Lₛ0= LLₛ > L (capped at L)Negative value
Moment of Inertia Ix1 mm⁴0 or negative
Section Modulus Sx1 mm³Sx > Zx (physically impossible)0 or negative
Yield Strength F₵100 MPa700 MPaF₵ < 235 MPa or > 460 MPa0 or negative
Elastic Modulus E100,000 MPa300,000 MPaE ≠ 200,000 ±10%0 or negative
Point Load P0Negative value
Load Position a0= La > L (capped to L)Negative value
Dynamic Load Factor1.03.0DLF > 2.5 (unusual)< 1.0 (meaningless)
Deflection LimitL/50L/1000Ratio < 50 (too lenient)
The calculator will show an alert dialog if a required field is empty or invalid before running any calculation. Fields highlighted in orange border indicate values outside the typical engineering range — calculation still proceeds but with a caution note in the results.

Load Combinations — LRFD vs ASD Explained

The calculator supports two design philosophies. Toggle Apply LRFD factors to switch between them.

LRFD (Load and Resistance Factor Design)

LRFD multiplies loads by partial factors that reflect their uncertainty, and multiplies material capacity by a resistance factor (ϕ < 1.0) to account for material variability. The governing combination used by the calculator is:

AISC LRFD Load Factors (ASCE 7)
\[1.4D\]
\[1.2D + 1.6L + 0.5(L_r \text{ or } S \text{ or } R)\]
\[1.2D + 1.6(L_r \text{ or } S \text{ or } R) + (L \text{ or } 0.5W)\]
\[0.9D + 1.0W\]
The calculator applies 1.2 × D loads + 1.6 × L loads automatically. Dead load factor = 1.2, Live = 1.6, Wind = 1.0, Snow = 1.6.

ASD (Allowable Stress Design)

ASD uses unfactored service loads and compares resulting stresses to allowable values. No load factors are applied (DLF = 1.0 for load effects). The safety margin is embedded in the allowable stress:

ASD Allowable Bending Stress
\[F_b = \frac{F_y}{1.67} = 0.6\,F_y\]
When LRFD toggle is OFF, the calculator reports the ASD Safety Factor directly. SF ≥ 1.67 = PASS. This is equivalent to σₛ ≤ 0.6 F₵.
Load TypeLRFD FactorASD FactorDescription
Dead (D)1.21.0Permanent loads: beam weight, slab, fixed equipment
Live (L)1.61.0Occupancy loads: people, furniture, movable equipment
Snow (S)1.61.0Ground or roof snow loads
Wind (W)1.01.0Lateral wind pressure (also roof uplift)
Self-weight1.2 (as D)1.0Auto-calculated from section weight kg/m

Steel Section Database — How to Read Section Properties

The Section DB tab lists all available sections with their structural properties. Understanding these values helps you make better section choices.

N.A. d (depth) b, (flange width) t, (flange thk) tw (web thk) W-SHAPE (I-Beam) centroid

Fig. 2 — W-shape (wide flange) cross-section dimensions: d (depth), b, (flange width), t, (flange thickness), tw (web thickness). The neutral axis (N.A.) passes through the centroid at mid-depth for symmetric sections.

Property Symbol Unit Physical Meaning Effect on Beam
DepthdmmOverall section heightLarger d ↑ more I, more σ arm
Flange Widthb,mmWidth of top/bottom flangesWider flange ↑ LTB resistance ↑
AreaAmm²Total cross-sectional areaProportional to weight (A×density)
Moment of InertiaIxmm⁴Resistance to bending curvatureHigher Ix ↑ less deflection, lower σ
Elastic Section ModulusSxmm³Ix / (d/2): elastic bending capacityHigher Sx ↑ lower bending stress
Plastic Section ModulusZxmm³Full plastic moment capacityZx > Sx; used in LRFD Mp = Fy×Zx
Weak-axis Gyrationrymm√(Iy/A): LTB slendernessHigher ry ↑ longer Lp, less LTB risk
Self-weightWkg/mMass per unit lengthIncluded as dead load (×9.81/1000 kN/m)

Application Presets — What Each One Pre-Loads

Each preset in the Presets tab auto-fills typical engineering values for that application type. You should verify and adjust values for your specific project.

Preset Span Section Loads Pre-filled DLF Def. Limit
 Residential Balcony 2.5 m W250x33 1.0 kN/m Dead + 2.4 kN/m Live (IBC residential) 1.0 L/360
 Canopy / Awning 3.0 m W200x22 0.5 kN/m Dead + 1.2 kN/m Snow 1.0 L/240
⛽ Swing Set Arm 2.0 m W150x22 2.5 kN tip point load (Live) 2.0 L/240
 Jib Crane Arm 4.0 m W310x33 20 kN tip load (Live) 1.5 L/240
 Signboard Bracket 1.5 m W150x13 0.5 kN/m Dead + 1.0 kN tip Wind load 1.0 L/180
 Deck Overhang 2.0 m W200x22 1.5 kN/m Dead + 2.0 kN/m Live 1.0 L/360
 Mezzanine Edge 3.0 m W310x52 2.0 kN/m Dead + 3.6 kN/m Live (office) 1.0 L/360
 Workshop Shelf 1.5 m W150x22 0.5 kN/m Dead + 5 kN tip Live 1.0 L/240
Always verify preset values against your actual project loads. The preset loads are based on typical design values and code minimums — your specific site conditions, local code requirements, and actual tributary areas may require different values. A structural engineer should confirm loads for safety-critical applications.

 Accuracy Statement & Limitations

This calculator implements Euler-Bernoulli beam theory with Kirchhoff assumptions (small deflections, linear elastic material, prismatic cross-section, plane sections remain plane). It is calibrated against AISC Steel Construction Manual examples and gives results within ±1% of hand calculations for the covered load cases.

Scope of calculations:

  • Prismatic (uniform cross-section) steel beams only
  • Linear elastic behavior (no plastic redistribution for continuous cantilevers)
  • Euler-Bernoulli theory: shear deformation ignored (valid when L/d > 10)
  • LTB uses AISC F2 equations with Cₛ = 1.0 (conservative for cantilevers)
  • Deflection uses superposition of closed-form solutions — exact for the listed load types
  • Shear deformation not included — may underestimate deflection by 3–10% for deep, short sections

This tool is intended for preliminary design and educational purposes only. Final structural designs for buildings, public structures, or any safety-critical application must be reviewed and stamped by a licensed Professional Engineer (PE) or Chartered Engineer (CEng) who takes professional responsibility for the design.

Frequently Asked Questions (FAQ)

Answers to the most common questions about cantilever beam design and how to use this calculator.

There is no single maximum — it depends on load, section, and deflection limit. Practical steel cantilever spans typically range:

  • Residential balconies: 1.5 – 3.0 m (W200 to W310 sections)
  • Commercial canopies: 2.0 – 6.0 m (W310 to W460 sections)
  • Industrial crane arms: 3.0 – 10.0 m (W460 to W610 and above)

For long spans, deflection (L/360 check) typically governs before strength. Use the Optimize tab to find the minimum section for your specific span and load.

This can happen because DCR uses factored (LRFD) loads (1.2D + 1.6L) compared to ϕMₙ, while the Safety Factor (ASD) uses unfactored service loads compared to F₵. The LRFD method applies higher safety margins and is the more conservative check. If DCR bending > 1.0, the beam fails AISC 360 LRFD — regardless of the ASD safety factor. You should resize the section to bring DCR ≤ 1.0.

Lateral-Torsional Buckling (LTB) is when the compression flange of the beam buckles sideways before the section can develop its full plastic moment. "Inelastic LTB" means the unbraced length Lₛ is between Lₚ and Lᵣ — the section develops some plastic capacity but not the full Mₙ. Solutions:

  • Add lateral bracing along the compression flange to reduce Lₛ
  • Use a section with a wider flange (larger b,) for better LTB resistance
  • Increase the section size (larger rₖ increases Lₚ)
  • Use an HSS section (closed section has much better torsional resistance)

This calculator is optimised for steel beams only. However, you can use it for reinforced concrete by entering a custom section with the appropriate transformed Iₓ for the cracked section, and using E = 30,000 MPa (typical for concrete). Note that:

  • The LTB check is not applicable to concrete (no lateral buckling of compression zone)
  • The yield strength F₵ should not be interpreted as reinforcement yield — instead compare σₛ against 0.45fʹс (ACI) for compression, or use moment capacity from ACI 318 separately
  • Long-term creep deflection in concrete is not included — multiply deflection by 2.0–3.0 for sustained loads

For a full concrete cantilever analysis, use a dedicated RC beam calculator.

Always defer to a licensed local engineer. This calculator:

  • Does not account for local code amendments that may require higher load factors
  • Does not check connection details (welds, bolts at the fixed support)
  • Does not account for notches, holes, or fabrication imperfections
  • Does not model partial fixity (assumes perfectly rigid connection at wall)
  • May use different load models than required by your local authority

Use this tool for preliminary sizing and educational understanding. The engineer of record (EOR) who stamps the drawings is legally responsible for the final design.

Multiply the area pressure (kN/m²) by the tributary width (m) of the beam:

w [kN/m] = q [kN/m²] × tributary width [m]

Example: 2.4 kN/m² live load on a 1.5 m wide balcony = 3.6 kN/m on the cantilever beam. For two beams sharing the load, tributary width = 1.5/2 = 0.75 m, giving 1.8 kN/m per beam.

W250x25 is a North American W-shape per AISC; IPE 240 is a European parallel-flange I-section per Eurocode. Key differences:

  • W-shapes have slightly thicker flanges relative to web, optimised for US practice. Used with AISC 360.
  • IPE sections have tapered flanges (narrower at tips) and are lighter per unit depth. Used with Eurocode 3.
  • W250x25: Ix = 48.7×10⁶ mm⁴, W = 25 kg/m. IPE 240: Ix = 38.9×10⁶ mm⁴, W = 30.7 kg/m.
  • Use W-shapes if procuring in North America; use IPE if sourcing in Europe/Asia.

Yes, best practice is to target DCR ≤ 85–90% for serviceability checks like deflection. A 98% DCR leaves almost no margin for:

  • Load variability (actual loads often exceed nominal values)
  • Connection flexibility (real fixity is never 100% — adds to deflection)
  • Long-term effects (permanent dead loads cause creep deflection over time)
  • Future load changes (added weight, changed use)

Use the Optimize tab to find the next available section with a more comfortable margin. The additional cost of one size up is almost always worth the reliability.

On the Results tab, use the Print / Export PDF button (calls browser print dialog, save as PDF). This captures:

  • All input parameters with units
  • Complete results table with pass/fail for every check
  • Step-by-step derivation showing all formulas and intermediate values
  • Demand/Capacity ratios

For official permit submissions, the PDF should be accompanied by a cover sheet from the Engineer of Record (EOR) confirming the design parameters and taking professional responsibility. Many jurisdictions require a PE/CEng stamp on structural calculations submitted with permit applications.

Yes — use the Back-Span Length input to model this. When a back-span is entered:

  • The calculator computes the uplift reaction at the back-span anchor (holds-down force required at the far support)
  • The cantilever portion is still analyzed as a pure fixed-free cantilever for deflection and stress
  • You should also manually check the back-span portion separately (simply supported, same loads) using the deflection formula δ = 5wL⁴/384EI

For a full continuous beam analysis with multiple spans, you will need a more advanced tool such as a moment-distribution calculator or FEA software.

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