Calculator
Stair Waist Slab Calculator
Waist thickness and self-weight from flight span.
- Waist
- 150 mm
- L/25 rule
Live statistics
140 mm
150 mm
3.75 kPa
Support centres.
How you compare — standard sections
| Section | Depth (mm) | Mass (kg/m) | A (cm²) | Iₓ (×10⁶ mm⁴) | Sₓ (×10³ mm³) |
|---|---|---|---|---|---|
| UB 305×165×40 · Steel I-beam | 304 | 40.3 | 51.3 | 85 | 560 |
| UB 457×191×67 · Steel I-beam | 454 | 67.1 | 85.5 | 294 | 1290 |
| UC 254×254×73 · Steel column | 254 | 73.1 | 93.1 | 114 | 895 |
| RC 300×500 (C30) · Concrete beam | 500 | 375 | 1500 | 3125 | 12500 |
| Glulam 140×450 · Timber beam | 450 | 29 | 630 | 1063 | 4725 |
| SHS 200×200×8 · Hollow section | 200 | 47.4 | 60.4 | 36.9 | 369 |
Indicative values for scheme design only. Always verify against the manufacturer / code tables (AISC Steel Manual, SCI Blue Book, ACI detailing) before ordering steel or pouring concrete.
Plans & details
Stair detail
Riser, tread, waist and landing per code.
Plan sketch
Verify rise, going and headroom.
Site verification
Check levels, cover and bearings.
Typical details for scheme design. Replace placeholders with project drawings (1200×630 JPG or SVG line work in /public/plans/civil/). Do not scale from web images — use figured dimensions.
Design verification checklist
Work through before issuing results — 1/6 verified (17%).
Results
Exact waist
140mm
Span times 1000 over 25.
150mm
Rounded up to 25 mm.
3.75kPa
25 times use thickness over 1000.
Visualizations
Results Overview
Formula
Span-over-25 rule gives a deflection-safe starting waist, rounded for formwork with its self-weight.
Alternative Form
Variables
| Symbol | Name | Unit | Description |
|---|---|---|---|
| span | Flight span | m | Support centres. |
| t | Waist thickness | mm | Normal to soffit. |
| self | Self-weight | kPa | Slab only. |
Explanation
Span over 25 with formwork rounding plus self-weight.
Derivation
Empirical deflection control for one-way stair slabs: depth near span over 25 limits sag and vibration at scheme.
Step-by-Step Calculation
Follow each step to understand how the result is calculated from your inputs.
Enter flight span
Read exact and use waist
Carry self-weight to loads
Worked Examples
See how the calculator works with different scenarios.
Scenario
Dog-leg waist.
Inputs
Calculation
t is 3500/25 = 140 mm, so use 150 mm. Self-weight is 3.75 kPa.
Result
Use 150 mm waist
Interpretation
Effective depth near 125 mm after cover; check moment next.
Understanding Your Result
Your Result: Exact waist = 140 mm · Use waist = 150 mm · Slab self-weight = 3.75 kPa
Typical range: 125-175 mm for 3-4 m flights.
What This Means
Starting waist depth that usually deflects acceptably.
Why It Matters
Thin waists bounce and crack; this rule avoids rework.
Professional Interpretation
Adopt the rounded waist then prove moment, shear and deflection.
Recommendations
- •Keep 2R+T 600-640
- •Verify headroom 2m+
- •Verify one line by hand
Learn — structural behaviour, deeply
Span in, thickness out.
1 · The two equations that run every site
ΣF_y = 0
Vertical balance
Upward reactions must equal total downward load. Missing 1 kN here means a 1 kN shear error everywhere downstream.
ΣM = 0
Moment balance
Moments about ANY point must cancel. Take moments about one support to eliminate it and solve the other directly.
ΣF_x = 0
Horizontal balance
Zero for vertical-only loading — but the pin still needs checking once wind, soil or inclined loads appear.
2 · Support types — what each one can (and cannot) do
| Support | Reactions | Allows | Watch out |
|---|---|---|---|
| Roller | 1 (vertical) | Horizontal slide + rotation | Provides NO lateral restraint — pair with a pin or bracing. |
| Pin / hinge | 2 (vertical + horizontal) | Rotation only | Moment released here — detail the hinge, never weld it rigid by accident. |
| Fixed / clamped | 3 (+ moment) | Nothing (fully restrained) | Attracts large moments; settlement or temperature causes locked-in stress. |
| Propped cantilever | 3 (indeterminate ×1) | Rotation at prop | Needs compatibility (deflection = 0 at prop) — equilibrium alone is not enough. |
| Continuous (3+ supports) | 4+ (indeterminate) | Rotation over interior piers | Solve by superposition / moment distribution / software; reactions shift with stiffness. |
3 · Factor-impact table — what moves your reactions most
| Factor | Typical impact | Why |
|---|---|---|
| Load position (a/L) | Linear, dominant | Moving P toward a support shifts ~100% of P onto it. Ra = P·(L−a)/L — position matters more than span. |
| UDL intensity (w) | ∝ w·L total | Each extra 1 kN/m on a 6 m beam adds 3 kN per reaction. Self-weight alone is often 1–5 kN/m on concrete. |
| Span length (L) | ∝ L for UDL | Doubling L doubles UDL reactions and quadruples UDL moment (wL²/8). Keep spans tight where possible. |
| Overhang length (c) | ∝ c/L uplift | Uplift at the far support = P·c/L. A 2 m overhang with 10 kN on a 5 m span pulls down 4 kN — needs hold-down. |
| Fixity (pinned → fixed) | Redistributes ~10–30% | Fixed ends attract moment and shed midspan moment. Never assume fixity you have not detailed. |
| Support settlement (Δ) | 0 (det.) / large (indet.) | Determinate beams just rotate; continuous/fixed beams develop locked-in moments ≈ 3EIΔ/L². |
| Dynamic / impact | +10–100% | Static reactions must be amplified for cranes, machinery, footfall (see ASCE 7 Ch. 4, AISC DG11). |
| Load combination | × 1.2–1.6 (LRFD) | 1.2D + 1.6L + 0.5(Lr/S/R) governs most beams. Reactions for strength ≠ reactions for service checks. |
4 · Code provisions you must cite on drawings
- ASCE 7 load combinations (LRFD): 1.4D · 1.2D + 1.6L + 0.5(Lr/S/R) · 1.2D + 1.0W + 1.0L … Strength reactions use factored loads; bearing/deflection checks use service (unfactored) loads.
- ACI 318 (concrete): strength-reduction ϕ = 0.65–0.90; development/lap lengths Ch. 25; one-way shear + punching Ch. 22. Reactions feed directly into Vu ≤ ϕVn.
- AISC 360 (steel): Ch. F/G/H for moment/shear/combined; bearing at supports per J7–J8; bracing per App. 6. Connection must develop the computed reaction — a beam is only as strong as its seat.
- Eurocode basis (EN 1990): ULS 1.35G + 1.5Q; SLS G + Q (characteristic). National annexes adjust factors — confirm the project annex.
- Serviceability (all codes): live-load deflection ≈ L/360 floors, L/240 roofs; total ≈ L/240. Vibration: AISC DG11 / SCI P354 for rhythmic or office floors.
5 · Pro workflow (5 minutes per beam)
- Sketch the free-body diagram: every load incl. self-weight, every support, dimensions.
- Solve ΣM then ΣF — write both lines on the calc sheet so a checker can follow.
- Verify: re-take moments about the OTHER support; residual must be ≈ 0.
- Draw shear then moment (reactions are the SFD starting values).
- Size the support: bearing stress, padstone, bolt/weld group, foundation pressure.
- File: keep the input → reaction → SFD/BMD → support chain on one page.
6 · Field traps (where reactions go wrong)
- • Forgetting self-weight: a 300×600 concrete beam weighs 4.5 kN/m — on 6 m that is 13.5 kN per support.
- • Assuming fixity: a “fixed” sketch with two bolts is a pin. Model what you detail.
- • Ignoring uplift: overhang + wind can reverse a bearing — light roofs lift off.
- • Mixing factored/service: never compare a factored reaction against an allowable soil pressure.
- • Point load at the wrong station: 0.5 m error on a 10 kN load swings reactions by P·Δa/L.
7 · The 3-check rule (sign-off standard)
- Math check: ΣFy and ΣM both close to zero with project units printed.
- Sanity check: reactions sum to total load; heavier side sits under heavier load; UDL symmetry gives Ra ≈ Rb.
- Load-path check: every reaction lands on something sized for it — beam → seat → column → footing → soil, no floating numbers.
Practical Tips
- •Split dead vs live early — factoring depends on it
- •Include self-weight; concrete often dominates
- •Report service values to 1 decimal for bearings and footings
Common Mistakes
Assumptions
This calculator makes the following assumptions to provide estimates:
Limitations
Be aware of these limitations when using this calculator:
Frequently Asked Questions
Answers to common questions about this calculator.
Why 25 mm rounding?
Does landing count in span?
What about long spans?
Is this final?
How do I find reactions for a simply supported beam?
What does a negative (downward) reaction mean?
Do I include the beam self-weight?
Service vs factored loads — which do I report?
What is the difference between a UDL and a UVL?
How do I turn a floor area load into a beam line load?
What is tributary area?
Which load combination usually governs a beam?
LRFD vs ASD — does it change the reactions?
Pin, roller or fixed — how do I choose the support model?
What deflection limits apply to beams?
How do I convert kN ↔ kips and m ↔ ft?
Shear vs bending moment — which sizes what?
Where does the maximum moment occur?
What is section modulus and how do I use it?
How do I quickly check a steel beam?
How do I quickly check a concrete beam?
What is development length and why does it matter?
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Glossary
Technical terms used in mortgage calculations explained in plain language.
- Reaction
- Force (or moment) a support exerts on a member to maintain static equilibrium (ΣF = 0, ΣM = 0).
- Simply supported
- Beam on one pin + one roller. Resists vertical load; allows rotation and (at roller) horizontal movement.
- Fixed support
- Clamped end resisting force AND moment; prevents rotation. Used in cantilevers and fixed frames.
- UDL / UVL
- Uniformly distributed load (constant kN/m) vs. uniformly varying load (triangular, zero-to-max).
- Tributary area
- Floor/roof area whose load drains to one member. Line load = area load × tributary width.
- Factored load
- Service load × LRFD load factor (e.g. 1.2D + 1.6L) for strength design per ASCE 7.
- Serviceability
- Deflection, cracking and vibration limits under day-to-day (unfactored) loads.
- Uplift
- Net downward-hold requirement: a negative (downward-pulling) reaction, common on overhangs.
Authoritative References
Trusted sources and standards referenced by this calculator.
Applicable Standards
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2026-09-28
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