Checks a strip of reinforced concrete slab under uniform, partial and line loads in service, to SIA 262:2025: the moments of the load combinations, concrete compression and creep, bar stresses and crack control, crack width, long-term deflection with cracking, creep and shrinkage, finishes, comfort and natural frequency. Every step shows its formula and the clause it comes from.
What it checks
- Load combinations: the self-weight g1 = γRC · h is added to the loads entered; for each combination, ΣF, RA, RB, MA = −ηA · M0,max, Mmax at xM and MB = −ηB · M0,max, per metre of width, then Mqp, Mfr and Mra at the critical sections.
- Section per metre of width: as and a′s, d and d′sup, with fcm = fck + 8, clause 3.1.2.2.3, equation (6).
- Cracking moments Mcr and M′cr (4.2.1.14), with fct,eff = kt · fctm, clause 4.4.1.3, equations (99) and (100).
- Concrete compression, check 1: σc,qp ≤ 0.6 · fcm (3.1.2.6.3).
- Bar stresses in the span and over the support against σs,adm = √(9 · Es · fctm · wnom / Øs) ≤ fyk, clause 4.4.2.3.4, equation (102), with wnom from Table 17: at first cracking (minimum reinforcement, 4.4.2.3.3) and under the quasi-permanent load.
- No yielding: σs,ra ≤ fyd − 80 N/mm² under the characteristic combination (Table 17).
- Crack width (optional) to EN 1992-1-1 §7.3.4, equations (7.8) to (7.11), against wmax.
- Deflection: wc (4.4.3.2.4), the estimates wcφ = wc · (1 + φ), equation (103), and w104 = (1 − 20 · ρ′)/(10 · ρ^0.7) · (0.75 + 0.1 · φ) · (h/d)³ · wc, clause 4.4.3.2.5, equation (104), and a detailed calculation of the curvatures along the span to EN 1992-1-1 §7.4.3, equations (7.18) to (7.21).
- Deflection limits (4.4.3.2.1): w∞ for appearance, Δw = w∞ − wg1,0 for finishes and partitions, and wq,fr under ψ1 · qk for comfort.
- Natural frequency f1 ≥ fmin (4.4.4.2), from the Rayleigh quotient of the static deflection curve.
What you enter and what you get
You enter the static system (simply supported, fixed at one or both ends, or a span of a continuous member with the support moments ηA and ηB as fractions of M0, the largest moment of the same loads on a simple span), the span l and, for a panel spanning both ways, the share α of the load carried by this strip. Then h, the bottom bars Ø at s with cover c, the top bars Ø′ at s′ with cover c′, whether the top bars run through the span, the materials, the creep and shrinkage data and the faces exposed to drying. You enter up to five uniform loads, each on the whole span or on a part of it, and up to five line loads across the strip at x1, each with a permanent and a variable part (g2,1 and q1, G1 and Q1 for the first), then ψ1 and ψ2, the requirement level, the crack width option and the deflection limits as fractions of the span.
You get φ and εcs, the section stiffnesses, the support forces and moments of each load combination, the moments at the critical sections, every check with its utilisation and clause, and both deflection estimates. With the Basic plan, it prints as an A4 calculation note.
Assumptions and limits
- Moments come from an elastic, uncracked analysis; the redistribution caused by cracking is not followed.
- ηA and ηB apply to every load combination: take them from an elastic analysis of the continuous member under a similar layout of the loads.
- A line load is entered in kN per metre of width; a load on a small area is entered divided by the width over which it is spread.
- A two-way panel is checked as a beam strip under α · p, with α from your plate analysis.
- The bottom bars are assumed to run to the supports.
- φ follows EN 1992-1-1 Annex B and εcs EN 1992-1-1 §3.1.4, or your own values. The notional size h0 = 2 · Ac/u counts only the faces exposed to drying.
- Equation (104) is an upper bound (4.4.3.2.6). The detailed calculation is the detailed study of 4.4.3.2.3.
- For finishes, the creep under g1 before they are placed is counted as occurring after, on the safe side.
Worked example
A 240 mm slab, end span of a continuous slab with l = 6 m, Ø12 at 150 mm at the bottom and Ø14 at 150 mm over the support, fck = 30 N/mm², g2,1 = 2 kN/m² and q1 = 2 kN/m² on the whole span, a further q2 = 2 kN/m² from 3 m to 6 m, a permanent line load G1 = 4 kN/m at 2 m, increased requirements, wmax = 0.3 mm and fmin = 5 Hz. These are the module's own results for its worked example, computed when this page was built.
Inputs| Input | Value | Ref. |
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| Support conditions of the span | Span of a continuous member | |
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| Moment at the left support, fraction of M0 ηA | 0 | |
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| Moment at the right support, fraction of M0 ηB | 1 | |
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| Span l | 6 m | |
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| Slab thickness h | 240 mm | |
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| Bottom bars: diameter Ø | 12 mm | |
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| Bottom bars: spacing s | 150 mm | |
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| Bottom bars: concrete cover c | 30 mm | |
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| Top bars over the supports: diameter Ø′ | 14 mm | |
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| Top bars over the supports: spacing s′ | 150 mm | |
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| Top bars: concrete cover c′ | 30 mm | |
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| Do the top bars run through the span? | No | |
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| Characteristic compressive strength fck | 30 N/mm² | § 3.1.2.2.2 |
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| Mean tensile strength fctm | 2.9 N/mm² | § 3.1.2.2.4 |
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| Modulus of elasticity Ecm | 32000 N/mm² | § 3.1.2.3.3 |
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| Unit weight of reinforced concrete γRC | 25 kN/m³ | |
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| Characteristic yield strength fyk | 500 N/mm² | |
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| Modulus of elasticity Es | 205000 N/mm² | |
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| Resistance factor for steel γs | 1.15 | § 2.4.2.6 |
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| Creep coefficient φ | Computed (EN 1992-1-1 Annex B) | § 3.1.2.6 |
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| Relative humidity of the environment RH | 50 % | |
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| Cement class | N — normal hardening | |
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| Age of the concrete at loading t0 | 28 days | |
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| Age considered (service life) t | 50 years | |
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| Shrinkage strain εcs | Computed (EN 1992-1-1 §3.1.4) | § 3.1.2.7 |
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| Age at the end of curing ts | 7 days | |
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| Faces of the slab exposed to drying | Both faces | |
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| Number of uniform loads | 2 | |
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| Extent | Whole span | |
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| Permanent part g2,1 | 2 kN/m² | |
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| Variable part q1 | 2 kN/m² | |
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| Extent | Part of the span | |
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| Starts at, from the left support a2 | 3 m | |
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| Ends at, from the left support b2 | 6 m | |
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| Permanent part g2,2 | 0 kN/m² | |
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| Variable part q2 | 2 kN/m² | |
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| Number of line loads | 1 | |
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| Position, from the left support x1 | 2 m | |
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| Permanent part G1 | 4 kN/m | |
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| Variable part Q1 | 0 kN/m | |
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| Combination factor, frequent ψ1 | 0.5 | |
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| Combination factor, quasi-permanent ψ2 | 0.3 | |
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| Requirement level | Increased | § 4.4.2.2.3 |
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| Tensile strength for the first crack | Mean tensile strength (4.4.1.3) | § 4.4.1.3 |
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| Exposure to chlorides, frost or sea water? | No — X0 or XC | EN 1992-1-1 §7.2(2) |
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| Compute the crack width? | Yes | |
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| Bond of the bars k1 | High-bond bars (0.8) | EN 1992-1-1 §7.3.4(3) |
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| Crack spacing factor for the cover k3 | 3.4 | EN 1992-1-1 §7.3.4(3) |
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| Crack spacing factor for the bond length k4 | 0.425 | EN 1992-1-1 §7.3.4(3) |
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| Limiting crack width (optional) wmax | 0.3 mm | |
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| Deflection used in the checks | Detailed — curvatures along the span | § 4.4.3.2.3 |
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| Limit for appearance: l divided by l/wadm | 300 | § 4.4.3.1.1 |
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| Check the deflection after the finishes are placed? | Checked | |
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| Limit: l divided by l/wadm | 500 | § 4.4.3.2.1 |
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| Check the deflection under the frequent variable load? | Checked | |
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| Limit: l divided by l/wadm | 350 | § 4.4.3.2.1 |
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| Check the natural frequency? | Checked | § 4.4.4.1 |
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| Lowest admissible natural frequency fmin | 5 Hz | § 4.4.4.2 |
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Calculation: Self-weight| Step | Value | Ref. |
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| Self-weightγRC·h | g1 = 6.00 kN/m² | |
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Calculation: Load combinations and their moments| Step | 1Quasi-permanentg + ψ2·q | 2Frequentg + ψ1·q | 3Characteristicg + q | Ref. |
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| Total load on the span ΣF kN per mg1 + the loads of the combination | 57.4 | 61.0 | 70.0 | |
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| Force at the left support RA kN per m | 21.6 | 22.6 | 25.2 | |
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| Force at the right support RB kN per m | 35.8 | 38.4 | 44.8 | |
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| Moment at the left support MA kNm per m−ηA·M0,max | 0.0 | 0.0 | 0.0 | |
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| Largest moment in the span Mmax kNm per m | 25.9 | 27.3 | 30.6 | |
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| Its position, from the left support xM m | 2.04 | 2.07 | 2.12 | |
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| Moment at the right support MB kNm per m−ηB·M0,max | -44.1 | -46.8 | -53.5 | |
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Calculation: Section| Step | Value | Ref. |
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| Slab thicknessper metre of width, b = 1000 mm | h = 240 mm | |
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| Bottom barsπ·Ø²/4·1000/s — Ø12 @ 150 mm | as = 754 mm²/m | |
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| Effective depth of the bottom barsh − c − Ø/2 | d = 204 mm | |
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| Top bars over the supportsØ14 @ 150 mm | a′s = 1,026 mm²/m | |
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| Effective depth of the top bars (from the bottom face)h − c′ − Ø′/2 | d′sup = 203 mm | |
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Calculation: Materials| Step | Value | Ref. |
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| Mean compressive strengthfck + 8 | fcm = 38.0 N/mm² | § 3.1.2.2.3 (6) |
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| Design yield strength of the barsfyk/γs | fyd = 434.8 N/mm² | § 2.4.2.5 (4) |
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| Short-term modular ratioEs/Ecm | αe = 6.41 | |
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Calculation: Creep| Step | Value | Ref. |
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| Notional size2·Ac/u, u = 2,000 mm per metre | h0 = 240 mm | EN 1992-1-1 Annex B (B.6) |
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| Humidity factor[1 + (1 − RH/100)/(0.1·∛h0)·α1]·α2 | φRH = 1.731 | EN 1992-1-1 Annex B (B.3) |
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| Strength factor16.8/√fcm | β(fcm) = 2.725 | EN 1992-1-1 Annex B (B.4) |
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| Age at loading adjusted for the cementt0·(9/(2 + t0^1.2) + 1)^α ≥ 0.5, α = 0 | t0,adj = 28.0 days | EN 1992-1-1 Annex B (B.9) |
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| Age factor1/(0.1 + t0^0.2) | β(t0) = 0.488 | EN 1992-1-1 Annex B (B.5) |
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| Notional creep coefficientφRH·β(fcm)·β(t0) | φ0 = 2.304 | EN 1992-1-1 Annex B (B.2) |
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| Humidity–size coefficient1.5·[1 + (0.012·RH)^18]·h0 + 250·α3 ≤ 1500·α3 | βH = 600 days | EN 1992-1-1 Annex B (B.8) |
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| Development with time[(t − t0)/(βH + t − t0)]^0.3, t = 18,250 days | βc(t, t0) = 0.990 | EN 1992-1-1 Annex B (B.7) |
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| Creep coefficientφ0·βc(t, t0)valid for compressive stresses up to 0.45·fck at loading | φ(t, t0) = 2.28 | EN 1992-1-1 Annex B (B.1) |
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Calculation: Shrinkage| Step | Value | Ref. |
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| Humidity factor1.55·[1 − (RH/100)³] | βRH = 1.356 | EN 1992-1-1 Annex B (B.12) |
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| Basic drying shrinkage0.85·[(220 + 110·αds1)·exp(−αds2·fcm/10)]·10⁻⁶·βRH | εcd,0 = 0.482 ‰ | EN 1992-1-1 Annex B (B.11) |
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| Size coefficientfrom h0, linear between the values of Table 3.3 | kh = 0.810 | EN 1992-1-1 §3.1.4(6) |
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| Development of drying(t − ts)/[(t − ts) + 0.04·√h0³] | βds(t, ts) = 0.992 | EN 1992-1-1 §3.1.4 (3.10) |
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| Drying shrinkageβds·kh·εcd,0 | εcd = 0.387 ‰ | EN 1992-1-1 §3.1.4 (3.9) |
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| Final autogenous shrinkage2.5·(fck − 10)·10⁻⁶ | εca,∞ = 0.050 ‰ | EN 1992-1-1 §3.1.4 (3.12) |
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| Autogenous shrinkage[1 − exp(−0.2·√t)]·εca,∞ | εca = 0.050 ‰ | EN 1992-1-1 §3.1.4 (3.11) |
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| Total shrinkage strainεcd + εca | εcs = 0.437 ‰ | EN 1992-1-1 §3.1.4 (3.8) |
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Calculation: Cracking of the sections| Step | Value | Ref. |
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| Size factor1/(1 + 0.5·t), t = h/3 in m | kt = 0.962 | § 4.4.1.3 (100) |
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| Effective tensile strengthkt·fctmfor the cracking moments and the deflection | fct,eff = 2.79 N/mm² | § 4.4.1.3 (99) |
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| Cracking moment, span section (sagging)fct,eff·II/(h − yI), uncracked section with αe | Mcr = 27.8 kNm | § 4.2.1.14 |
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| Cracking moment, support section (hogging)fct,eff·II/yI, tension at the top face | M′cr = 28.4 kNm | § 4.2.1.14 |
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Calculation: Stiffness of the sections| Step | Value | Ref. |
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| Effective long-term modulusEcm/(1 + φ)φ of the creep part above; increased later if the concrete stress exceeds 0.4·fcm | Ec,eff = 9,751 N/mm² | EN 1992-1-1 §7.4.3 (7.20) |
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| Long-term modular ratioEs/Ec,eff | αe,∞ = 21.02 | |
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| Gross concrete section, spanb·h³/12 | Ic = 1,152 10⁶ mm⁴ | |
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| Uncracked section, long term, spanconcrete + αe,∞·bars | II = 1,252 10⁶ mm⁴ | |
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| Cracked section, long term, spancompressed concrete + αe,∞·barsneutral axis xII = 66 mm from the top | III = 398 10⁶ mm⁴ | |
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| Uncracked section, long term, support | I′I = 1,399 10⁶ mm⁴ | |
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| Cracked section, long term, supportcompression at the bottom; xII = 69 mm from the bottom | I′II = 513 10⁶ mm⁴ | |
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Calculation: Bending moments at the critical sections| Step | Value | Ref. |
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| Span (x = 2.13 m)cracked: |Mra| > Mcr = 27.8 kNm | Mqp ; Mfr ; Mra = 25.9 ; 27.2 ; 30.6 kNm | |
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| Right supportcracked: |Mra| > Mcr = 28.4 kNm | Mqp ; Mfr ; Mra = -44.1 ; -46.8 ; -53.5 kNm | |
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Calculation: Check 1 — concrete compression under the quasi-permanent load| Step | Value | Ref. |
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| Largest compression at loading (right support)cracked section, Ecm | |σc,qp| = 10.14 N/mm² | |
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| Stress–strength ratio | |σc|/fcm = 0.267 | |
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| Concrete compression within the range of the creep model|σc,qp|/(0.6·fcm) | η = 0.445 · Pass44 % of the capacity used | § 3.1.2.6.3 |
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Calculation: Admissible bar stress| Step | Value | Ref. |
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| Nominal crack widthincreased requirements | wnom = 0.5 mm | Table 17 |
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| Admissible bar stress, span√(9·Es·fctm·wnom/Øs) ≤ fyk, Øs = 12 mm | σs,adm = 472 N/mm² | § 4.4.2.3.4 (102) |
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| Admissible bar stress, right support√(9·Es·fctm·wnom/Øs) ≤ fyk, Øs = 14 mm | σs,adm = 437 N/mm² | § 4.4.2.3.4 (102) |
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Calculation: Check 2 — bar stress when the section cracks, span| Step | Value | Ref. |
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| Cracking moment for the first crackwith fct,eff = kt·fctm | Mcr = 27.8 kNm | § 4.4.1.3 |
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| Bar stress just after crackingcracked section under Mcr, Ecm | σs,r = 193 N/mm² | |
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| Bar stress at first cracking (minimum reinforcement)σs,r/σs,adm | η = 0.409 · Pass41 % of the capacity used | Table 17 |
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Calculation: Check 3 — bar stress when the section cracks, right support| Step | Value | Ref. |
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| Cracking moment for the first crackwith fct,eff = kt·fctm | Mcr = 28.4 kNm | § 4.4.1.3 |
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| Bar stress just after crackingcracked section under Mcr, Ecm | σs,r = 148 N/mm² | |
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| Bar stress at first cracking (minimum reinforcement)σs,r/σs,adm | η = 0.338 · Pass34 % of the capacity used | Table 17 |
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Calculation: Check 4 — bar stress under the quasi-permanent load, span| Step | Value | Ref. |
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| Bar stress under the quasi-permanent loadcracked section, Ec,effcompression in the concrete -4.31 N/mm² (long term) | σs,qp = 189 N/mm² | |
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| Bar stress under the quasi-permanent loadσs,qp/σs,adm | η = 0.400 · Pass40 % of the capacity used | Table 17 |
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Calculation: Check 5 — bar stress under the quasi-permanent load, right support| Step | Value | Ref. |
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| Bar stress under the quasi-permanent loadcracked section, Ec,effcompression in the concrete -5.94 N/mm² (long term) | σs,qp = 242 N/mm² | |
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| Bar stress under the quasi-permanent loadσs,qp/σs,adm | η = 0.553 · Pass55 % of the capacity used | Table 17 |
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Calculation: Check 6 — no yielding of the bars, span| Step | Value | Ref. |
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| Bar stress under the characteristic combinationcracked section, Ecm | σs,ra = 213 N/mm² | |
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| Bar stress against fyd − 80 N/mm²σs,ra/(fyd − 80) | η = 0.599 · Pass60 % of the capacity used | Table 17 |
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Calculation: Check 7 — no yielding of the bars, right support| Step | Value | Ref. |
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| Bar stress under the characteristic combinationcracked section, Ecm | σs,ra = 278 N/mm² | |
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| Bar stress against fyd − 80 N/mm²σs,ra/(fyd − 80) | η = 0.784 · Pass78 % of the capacity used | Table 17 |
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Calculation: Check 8 — crack width, span (EN 1992-1-1 §7.3.4)| Step | Value | Ref. |
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| Depth of the effective tension areamin(2.5·(h − d) ; (h − x)/3 ; h/2) | hc,ef = 58 mm | EN 1992-1-1 §7.3.2(3) |
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| Effective tension areab·hc,ef | Ac,eff = 57,961 mm² | |
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| Effective reinforcement ratioAs/Ac,eff | ρp,eff = 1.30 % | EN 1992-1-1 §7.3.4 (7.10) |
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| Maximum crack spacingk3·c + k1·k2·k4·φ/ρp,eff, k2 = 0.5 (bending), c = 30 mm, φ = 12 mm | sr,max = 259 mm | EN 1992-1-1 §7.3.4 (7.11) |
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| Mean strain difference, steel to concrete[σs − kt·fct,eff/ρp,eff·(1 + αe·ρp,eff)]/Es ≥ 0.6·σs/Es, kt = 0.4 (long term)σs = σs,qp = 189 N/mm²; the lower limit governs | εsm − εcm = 0.553 ‰ | EN 1992-1-1 §7.3.4 (7.9) |
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| Crack widthsr,max·(εsm − εcm) | wk = 0.143 mm | EN 1992-1-1 §7.3.4 (7.8) |
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| Crack width against the limitwk/wmax | η = 0.477 · Pass48 % of the capacity used | EN 1992-1-1 §7.3.1 |
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Calculation: Check 9 — crack width, right support (EN 1992-1-1 §7.3.4)| Step | Value | Ref. |
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| Depth of the effective tension areamin(2.5·(h − d) ; (h − x)/3 ; h/2) | hc,ef = 57 mm | EN 1992-1-1 §7.3.2(3) |
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| Effective tension areab·hc,ef | Ac,eff = 56,961 mm² | |
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| Effective reinforcement ratioAs/Ac,eff | ρp,eff = 1.80 % | EN 1992-1-1 §7.3.4 (7.10) |
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| Maximum crack spacingk3·c + k1·k2·k4·φ/ρp,eff, k2 = 0.5 (bending), c = 30 mm, φ = 14 mm | sr,max = 234 mm | EN 1992-1-1 §7.3.4 (7.11) |
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| Mean strain difference, steel to concrete[σs − kt·fct,eff/ρp,eff·(1 + αe·ρp,eff)]/Es ≥ 0.6·σs/Es, kt = 0.4 (long term)σs = σs,qp = 242 N/mm² | εsm − εcm = 0.843 ‰ | EN 1992-1-1 §7.3.4 (7.9) |
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| Crack widthsr,max·(εsm − εcm) | wk = 0.197 mm | EN 1992-1-1 §7.3.4 (7.8) |
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| Crack width against the limitwk/wmax | η = 0.657 · Pass66 % of the capacity used | EN 1992-1-1 §7.3.1 |
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Calculation: Elastic deflection| Step | Value | Ref. |
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| Elastic deflection, gross concrete section∬ Mqp/(Ecm·Ic) dx dx, with the support conditionsquasi-permanent load, uncracked, short term | wc = 1.88 mm | § 4.4.3.2.4 |
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Calculation: SIA estimate| Step | Value | Ref. |
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| Creep coefficient usedfrom the section part | φ = 2.28 | |
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| Uncracked, with creepwc·(1 + φ)valid: the quasi-permanent moment stays below Mcr | wcφ = 6.17 mm | § 4.4.3.2.4 (103) |
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| Tension reinforcement ratioAs/(b·d)span section | ρ = 0.370 % | |
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| Compression reinforcement ratioA′s/(b·d) | ρ′ = 0.000 % | |
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| Largely cracked, with creep(1 − 20·ρ′)/(10·ρ^0.7)·(0.75 + 0.1·φ)·(h/d)³·wc | w104 = 15.10 mm | § 4.4.3.2.5 (104) |
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Calculation: Detailed calculation| Step | Value | Ref. |
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| Effective modulusEcm/(1 + φ) | Ec,eff = 9,751 N/mm² | EN 1992-1-1 §7.4.3 (7.20) |
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| Shrinkage strainfrom the section part | εcs = 0.437 ‰ | |
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| Distribution coefficient at the point of largest deflection1 − β·(Mcr/M)², β = 0.5 (sustained load); 0 where M ≤ Mcr | ζ = 0.000 | EN 1992-1-1 §7.4.3 (7.19) |
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| Deflection if uncracked everywherecurvatures M/(Ec,eff·II) + shrinkage | wI,∞ = 7.37 mm | |
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| Deflection if fully crackedcurvatures M/(Ec,eff·III) + shrinkage | wII,∞ = 26.57 mm | |
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| Part due to shrinkageεcs·αe·S/I, weighted by ζ | wcs = 1.58 mm | EN 1992-1-1 §7.4.3 (7.21) |
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| Long-term deflection, quasi-permanent loadκ = ζ·κII + (1 − ζ)·κI, integrated twice | w∞ = 7.19 mm | EN 1992-1-1 §7.4.3 (7.18) |
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| Instantaneous deflection under the self-weightEcm, cracking with β = 1 | wg1,0 = 1.12 mm | |
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Calculation: Check 1 — appearance: long-term deflection| Step | Value | Ref. |
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| Admissible deflectionl/300 | wadm = 20.0 mm | |
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| Long-term deflection for appearancew∞/wadm | η = 0.360 · Pass36 % of the capacity used | § 4.4.3.2.1 |
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Calculation: Check 2 — damage to finishes: deflection after they are placed| Step | Value | Ref. |
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| Deflection after the finishes are placedw∞ − wg1,0 | Δw = 6.07 mm | |
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| Deflection after the finishes are placedΔw/wadm | η = 0.506 · Pass51 % of the capacity used | § 4.4.3.2.1 |
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Calculation: Check 3 — comfort: deflection under the frequent variable load| Step | Value | Ref. |
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| Short-term deflection from ψ1·qkw(g + ψ1·qk) − w(g), Ecm, β = 1 | wq,fr = 0.23 mm | EN 1992-1-1 §7.4.3 |
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| Deflection under the frequent variable loadwq,fr/wadm | η = 0.013 · Pass1 % of the capacity used | § 4.4.3.2.1 |
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Calculation: Check 4 — natural frequency| Step | Value | Ref. |
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| Mass on the spanquasi-permanent loads/gdistributed as the loads are | m = 5,851 kg per m | |
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| Short-term deflection under that massEcm, cracking with β = 1 | wqp,0 = 1.79 mm | |
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| First natural frequency(1/2π)·√(g·Σm·w/Σm·w²), Rayleigh quotient of the static deflection curve | f1 = 13.26 Hz | |
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| Natural frequency above the limitfmin/f1 | η = 0.377 · Pass38 % of the capacity used | § 4.4.4.2 |
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How this module is verified
Verified clause by clause against SIA 262:2025 and against independent calculations used on real projects, before release.
Questions
Why is equation (103) valid in the worked example?
The quasi-permanent moment in the span, 25.9 kNm, stays below Mcr = 27.8 kNm. The distribution coefficient ζ at the point of largest deflection is then 0, and equation (104) gives an upper bound only.
Which deflection is used in the checks?
You choose. The detailed calculation follows the curvatures along the span. The SIA estimate takes equation (103) when the span stays uncracked, otherwise equation (104). Both are always shown.
Which plan includes this module?
The Basic plan, with its calculation note.
Related
Norm: SIA 262:2025 · Page updated: 5 November 2026