Checks a reinforced concrete floor carried by columns, to SIA 262:2025: bending and torsion from an elastic plate, punching at every column, detailing, bar stresses, crack width and deflection, and chooses the bars zone by zone. Every step shows its formula and the clause it comes from.
What it checks
- Bending resistance of the four layers, mxRd, myRd, m′xRd and m′yRd, clause 4.2.1.5, and the ductility x/d ≤ 0.5 · 435/fyd (4.1.4.2.6).
- Minimum reinforcement and detailing: mcr ≤ mRd (4.3.1.2), the spacing (5.5.3.1) and the weaker direction at least 20 % of the main one (5.5.3.2).
- Bending and torsion, clause 4.3.2.6, equations (34a) to (34d): mxd + |mxyd| ≤ mxRd and its three counterparts, at every point of the plate.
- Punching at every column, without punching reinforcement: Vd ≤ VRd,c = kr · τcd · dv · u, 4.3.6.3.1, equation (58), with kr from equation (59) and the slab rotation ψ from 4.3.6.4.2, equation (60), at level 3.
- Serviceability: each layer cracked or not against mcr, the bar stress σs against Table 17, the crack width to EN 1992-1-1 §7.3.4, and the long-term deflection wcφ = wc · (1 + φ), 4.4.3.2.4, equation (103), against wadm.
- Bars chosen zone by zone: the lightest option of your list that meets every selected criterion, per zone and per layer.
What you enter and what you get
You enter the outline of the floor, the support of each edge, and on a plan the columns, openings and concentrated loads, placed by clicking. Then the section and its bars, the materials, the resistance factors, qd and the service load q. The creep coefficient φ is entered or computed.
You get every check with a pass or fail and where it governs. The punching of the most used column is shown step by step, from Vd = Rd − qd · A (4.3.6.2.6) and u₀ at dv/2 (4.3.6.2.2, Figures 22 and 23) to bs (equation (61)) and msd. With the Basic plan, it prints as an A4 calculation note.
Assumptions and limits
- Moments come from an uncracked linear elastic plate held over the column areas (4.1.4.1): a statically admissible field, on the safe side.
- The columns of the model carry no bending. ke takes the simplified values of 4.3.6.2.5 (0.9 interior, 0.7 edge, 0.65 corner) or equation (57).
- The top bars are taken as present wherever they are needed: extend them far enough into the panel.
- φ follows equation (13), each factor from EN 1992-1-1 Annex B, which agrees with SIA 262 Table 4 and Figure 2. k3 and k4 are nationally determined; you enter them.
- Steel masses exclude laps and anchorages. Trimmer bars and integrity reinforcement against progressive collapse (4.3.6.1.3, 4.3.6.7) are not designed.
Worked example
A floor of 18.4 × 12.4 m with free edges on twelve 400 × 400 mm columns, 6.0 m apart, one opening of 1.2 × 0.8 m, h = 280 mm, Ø12 at 200 mm at the bottom and Ø16 at 150 mm at the top both ways, fck = 30 N/mm², qd = 15.3 kN/m², a quasi-permanent load of 8.9 kN/m² and wadm = 24 mm. 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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| Length of the floor in x lx | 18.4 m | |
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| Length of the floor in y ly | 12.4 m | |
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| Left edge (x = 0) | Free | |
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| Right edge (x = lx) | Free | |
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| Bottom edge (y = 0) | Free | |
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| Top edge (y = ly) | Free | |
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| Plan of the floor | {"o":8.2,8.2,1.2,0.8,"q":[],"c":[[0.2,0.2,0.4,0.4,0],[0.2,6.2,0.4,0.4,0],[0.2,12.2,0.4,0.4,0],[6.2,0.2,0.4,0.4,0],[6.2,6.2,0.4,0.4,0],[6.2,12.2,0.4,0.4,0],[12.2,0.2,0.4,0.4,0],[12.2,6.2,0.4,0.4,0],[12.2,12.2,0.4,0.4,0],[18.2,0.2,0.4,0.4,0],[18.2,6.2,0.4,0.4,0],[18.2,12.2,0.4,0.4,0]]} | |
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| Slab thickness h | 280 mm | |
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| Cover to the bottom bars c | 30 mm | |
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| Outer bottom layer | Bars along x | |
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| Diameter Øx | 12 mm | |
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| Spacing sx | 200 mm | |
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| Diameter Øy | 12 mm | |
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| Spacing sy | 200 mm | |
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| Top reinforcement | Bars along x and y | |
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| Cover to the top bars c′ | 30 mm | |
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| Outer top layer | Bars along x | |
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| Diameter along x Ø′x | 16 mm | |
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| Spacing along x s′x | 150 mm | |
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| Diameter along y Ø′y | 16 mm | |
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| Spacing along y s′y | 150 mm | |
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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 | 33600 N/mm² | § 3.1.2.3.3 |
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| Poisson's ratio ν | 0.2 | § 3.1.2.3.5 |
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| Largest aggregate size Dmax | 32 mm | § 4.3.3.2.1 |
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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 concrete γc | 1.5 | § 2.4.2.6 |
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| Resistance factor for steel γs | 1.15 | § 2.4.2.6 |
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| Duration factor ηt | 1.0 — both conditions of 4.2.1.3 met | § 4.2.1.3 |
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| Design load, uniform qd | 15.3 kN/m² | |
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| Method for the bending moments | Linear elastic plate (4.1.4.1) | § 4.1.4 |
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| Moments over the columns | Mean over the support strip bs | § 4.1.4.2 |
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| Reduction ke for the moment transfer ke | Simplified values (4.3.6.2.5) | § 4.3.6.2.4 |
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| Tensile strength for cracking | Mean tensile strength (4.4.1.3) | § 4.4.1.3 |
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| Requirement level | Normal | § 4.4.2.2.3 |
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| Uniform load in the load case q | 8.9 kN/m² | |
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| Load case | Quasi-permanent | Table 17 |
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| Creep coefficient φ | Computed from the concrete, the exposure and the ages | § 3.1.2.6.2 |
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| Mean compressive strength fcm | 38 N/mm² | § 3.1.2.2.3 |
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| Relative humidity of the surroundings RH | 50 % | |
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| Faces drying out | Both faces | |
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| Cement | Normal hardening (class N) | |
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| Age of the concrete at loading t0 | 28 days | |
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| Age considered t | 25000 days | |
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| Admissible deflection (optional) wadm | 24 mm | |
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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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| Duration of the load kt | Long-term or repeated (0.4) | EN 1992-1-1 §7.3.4(2) |
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| Bar options | [[10,200],[12,200],[12,150],[14,150],[16,150],[16,100],[20,100]] | |
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| Size of a design zone az | 1.0 m | |
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| Bending resistance, eq. (34) | Yes | § 4.3.2.6 |
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| Minimum reinforcement and detailing | Yes | § 4.3.1.2 |
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| Bar stress in service, Table 17 | Yes | Table 17 |
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| Crack width in service | No | EN 1992-1-1 §7.3.4 |
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| No cracking in service | No | § 4.4.1.3 |
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| Deflection limit | Yes | § 4.4.3.2 |
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| Admissible deflection wadm | 24 mm | § 4.4.3.1.1 |
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Calculation: Reinforcement per metre of width| Step | Value | Ref. |
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| Bottom bars along xπ·Ø²/4·1000/sØ12 at 200 mm | as,bx = 565 mm²/m | |
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| Effective depth, bottom bars along xh − c − (bars below) − Ø/2 | dbx = 244 mm | |
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| Bottom bars along yπ·Ø²/4·1000/sØ12 at 200 mm | as,by = 565 mm²/m | |
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| Effective depth, bottom bars along yh − c − (bars below) − Ø/2 | dby = 232 mm | |
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| Top bars along xπ·Ø²/4·1000/sØ16 at 150 mm | as,tx = 1,340 mm²/m | |
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| Effective depth, top bars along xh − c′ − (bars above) − Ø/2 | dtx = 242 mm | |
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| Top bars along yπ·Ø²/4·1000/sØ16 at 150 mm | as,ty = 1,340 mm²/m | |
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| Effective depth, top bars along yh − c′ − (bars above) − Ø/2 | dty = 226 mm | |
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Calculation: Design strengths| Step | Value | Ref. |
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| Factor for the brittleness of strong concrete(40/fck)^(1/3) ≤ 1 | ηfc = 1.000 | § 4.2.1.2 (26) |
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| Design compressive strength of the concreteηfc·ηt·fck/γc | fcd = 20.0 N/mm² | § 2.4.2.3 (2) |
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| Design shear stress limit0.3·√fck/γc | τcd = 1.10 N/mm² | § 2.4.2.4 (3) |
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| Design yield strength of the steelfyk/γs | fyd = 434.8 N/mm² | § 2.4.2.5 (4) |
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Calculation: Bending resistances per metre| Step | Value | Ref. |
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| Bottom bars along xas·fyd·(d − 0.85·x/2), 0.85·x = as·fyd/fcdx/d = 0.059 | mxRd = 58.5 kNm/m | § 4.2.1.5 |
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| Bottom bars along yas·fyd·(d − 0.85·x/2), 0.85·x = as·fyd/fcdx/d = 0.062 | myRd = 55.5 kNm/m | § 4.2.1.5 |
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| Top bars along xas·fyd·(d − 0.85·x/2), 0.85·x = as·fyd/fcdx/d = 0.142; tension on top | m′xRd = 132.5 kNm/m | § 4.2.1.5 |
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| Top bars along yas·fyd·(d − 0.85·x/2), 0.85·x = as·fyd/fcdx/d = 0.152; tension on top | m′yRd = 123.2 kNm/m | § 4.2.1.5 |
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Calculation: Check 1 — ductility of the compression zone| Step | Value | Ref. |
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| Deepest compression zone (top bars along y)(x/d)/(0.5·435/fyd) | η = 0.303 · Pass30 % of the capacity used | § 4.1.4.2.6 |
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Calculation: Check 2 — minimum reinforcement: resistance above the cracking moment| Step | Value | Ref. |
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| Cracking moment per metrekt·fctm·h²/6, kt = 1/(1 + 0.5·h/3) (h in m) | mcr = 36.2 kNm/m | § 4.4.1.3 (99) |
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| Bottom bars along xmcr/mxRd | η = 0.619 · Pass62 % of the capacity used | § 4.3.1.2 |
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| Bottom bars along ymcr/myRd | η = 0.652 · Pass65 % of the capacity used | § 4.3.1.2 |
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Calculation: Check 3 — spacing and transverse reinforcement| Step | Value | Ref. |
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| Spacing, bottom bars along xs/smax | η = 0.667 · Pass67 % of the capacity used | § 5.5.3.1 |
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| Spacing, bottom bars along ys/smax | η = 0.667 · Pass67 % of the capacity used | § 5.5.3.1 |
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| Spacing, top bars along xs/smax | η = 0.500 · Pass50 % of the capacity used | § 5.5.3.1 |
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| Spacing, top bars along ys/smax | η = 0.500 · Pass50 % of the capacity used | § 5.5.3.1 |
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| Bottom: weaker direction against 20 % of the main one0.2·as,main/as,tr | η = 0.200 · Pass20 % of the capacity used | § 5.5.3.2 |
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| Top: weaker direction against 20 % of the main one0.2·as,main/as,tr | η = 0.200 · Pass20 % of the capacity used | § 5.5.3.2 |
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Calculation: Check 4 — bending and torsion, elastic plate: eq. (34)| Step | Value | Ref. |
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| Finite element meshuncracked plate, ν = 0.20, held over the column areas | 29 × 21 plate elements | |
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| Moments over the columnsacross each column strip, as for msd of the punching check | mean over bs | § 4.1.4.2 |
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| Positive moments in x — bottom bars along xmxd+|mxyd|/mxRd | η = 0.679 · Pass68 % of the capacity used | § 4.3.2.6 (34a) |
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| Positive moments in y — bottom bars along ymyd+|mxyd|/myRd | η = 0.953 · Pass95 % of the capacity used | § 4.3.2.6 (34b) |
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| Negative moments in x — top bars along x−mxd+|mxyd|/m′xRd | η = 0.711 · Pass71 % of the capacity used | § 4.3.2.6 (34c) |
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| Negative moments in y — top bars along y−myd+|mxyd|/m′yRd | η = 0.738 · Pass74 % of the capacity used | § 4.3.2.6 (34d) |
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Calculation: Check 5 — punching at every column, slab without punching reinforcement| Step | Value | Ref. |
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| Effective depth for punchingmean of the two top layerssupport at the underside of the slab | dv = 234 mm | § 4.3.6.2.1 |
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| Aggregate factor | kg = 1.200 | § 4.3.3.2.1 (37) |
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| Column C1 (corner)Vd/VRd,c | η = 0.661 · Pass66 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C2 (edge)Vd/VRd,c | η = 0.815 · Pass82 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C3 (corner)Vd/VRd,c | η = 0.687 · Pass69 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C4 (edge)Vd/VRd,c | η = 0.811 · Pass81 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C5 (interior)Vd/VRd,c | η = 0.896 · Pass90 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C6 (edge)Vd/VRd,c | η = 0.840 · Pass84 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C7 (edge)Vd/VRd,c | η = 0.815 · Pass81 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C8 (interior)Vd/VRd,c | η = 0.902 · Pass90 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C9 (edge)Vd/VRd,c | η = 0.847 · Pass85 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C10 (corner)Vd/VRd,c | η = 0.662 · Pass66 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C11 (edge)Vd/VRd,c | η = 0.841 · Pass84 % of the capacity used | § 4.3.6.3.1 (58) |
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| Column C12 (corner)Vd/VRd,c | η = 0.648 · Pass65 % of the capacity used | § 4.3.6.3.1 (58) |
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Calculation: Punching in detail — column C8, the most used| Step | Value | Ref. |
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| Column reactionsum of the support forces of the plate under the column | Rd = 588.6 kN | |
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| Load inside the control sectionA = 0.390 m² | qd·A = 6.0 kN | § 4.3.6.2.6 |
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| Design punching forceRd − qd·A | Vd = 582.6 kN | |
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| Control perimeterat dv/2 from the column, straight parts ≤ 1.5·dv from the cornersFigures 22, 23 | u₀ = 2,335 mm | § 4.3.6.2.2 |
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| Reduction for the moment transferinterior columnregular flat slabs; otherwise use eq. (57) | ke = 0.90 | § 4.3.6.2.5 |
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| Effective control perimeterke·u₀ | u = 2,102 mm | § 4.3.6.2.3 |
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| Distance to zero moment, xfrom the plate, along x through the column | rsx = 1.29 m | § 4.3.6.4.8 |
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| Distance to zero moment, y | rsy = 1.30 m | § 4.3.6.4.8 |
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| Width of the support strip1.5·√(rsx·rsy) ≤ lmin | bs = 1.95 m | § 4.3.6.4.6 (61) |
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| Mean moment in the strip, bars along xmean of −mxd + |mxyd| over bs at the column face | msd,x = 83.1 kNm/m | § 4.3.6.4.8 |
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| Mean moment in the strip, bars along y | msd,y = 81.4 kNm/m | § 4.3.6.4.8 |
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| Slab rotation, x1.2·(rsx/d)·(fyd/Es)·(msd,x/m′xRd)^1.5level 3: factor 1.2 | ψx = 0.0070 | § 4.3.6.4.2 (60) |
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| Slab rotation, y1.2·(rsy/d)·(fyd/Es)·(msd,y/m′yRd)^1.5 | ψy = 0.0076 | § 4.3.6.4.2 (60) |
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| Coefficient1/(0.45 + 0.18·ψ·d·kg) ≤ 2ψ = max(ψx ; ψy) | kr = 1.199 | § 4.3.6.3.2 (59) |
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| Punching resistancekr·τcd·dv·u | VRd,c = 646.0 kN | § 4.3.6.3.1 (58) |
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Calculation: Creep coefficient| Step | Value | Ref. |
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| Notional size2·Ac/uboth faces dry: h0 = h | h0 = 280 mm | |
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| Humidity and size factor[1 + (1 − RH/100)/(0.1·∛h0)·α1]·α2SIA 262 Figure 2 | φRH = 1.693 | EN 1992-1-1 (B.3) |
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| Strength factor16.8/√fcmSIA 262 Table 4 | βfc = 2.725 | EN 1992-1-1 (B.4) |
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| Age at loading, adjusted for the cementt0·(9/(2 + t0^1.2) + 1)^α, α = 0at 20 °C | t0,eff = 28.0 days | EN 1992-1-1 (B.9) |
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| Age-at-loading factor1/(0.1 + t0^0.2)SIA 262 Figure 2 | β(t0) = 0.488 | EN 1992-1-1 (B.5) |
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| Development with time[(t − t0)/(βH + t − t0)]^0.3, βH = 660SIA 262 Figure 2 | β(t − t0) = 0.992 | EN 1992-1-1 (B.7) |
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| Creep coefficientφRH·βfc·β(t0)·β(t − t0)for concrete stresses up to 0.4·fcm; above, 3.1.2.6.3 increases it | φ(t, t0) = 2.24 | § 3.1.2.6.2 (13) |
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Calculation: Moments under the service load| Step | Value | Ref. |
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| Cracking moment per metrekt·fct·h²/6 | mcr = 36.2 kNm/m | § 4.4.1.3 |
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| Modular ratioEs/Ecm | αs = 6.10 | |
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Calculation: Bottom bars along x (span)| Step | Value | Ref. |
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| Service moment, with the twisting momentlargest at x = 9.40 m, y = 9.00 m | m + |mxy| = 23.1 kNm/m | |
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| State | uncracked (m ≤ mcr) | |
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Calculation: Bottom bars along y (span)| Step | Value | Ref. |
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| Service moment, with the twisting momentlargest at x = 8.20 m, y = 9.00 m | m + |mxy| = 30.8 kNm/m | |
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| State | uncracked (m ≤ mcr) | |
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Calculation: Top bars along x (supports, corners)| Step | Value | Ref. |
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| Service moment, with the twisting momentlargest at x = 18.00 m, y = 7.00 m | m + |mxy| = 54.8 kNm/m | |
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| State | cracked (m > mcr) | |
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| Neutral axis depth, cracked | xII = 55.3 mm | § 4.1.4.2.1 |
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| Concrete stress−2·m/(xII·z)compression negative | σc = -8.87 N/mm² | |
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| Bar stressm/(as·(d − xII/3)) | σs = 182.8 N/mm² | |
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Calculation: Top bars along y (supports, corners)| Step | Value | Ref. |
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| Service moment, with the twisting momentlargest at x = 7.00 m, y = 12.00 m | m + |mxy| = 52.9 kNm/m | |
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| State | cracked (m > mcr) | |
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| Neutral axis depth, cracked | xII = 53.2 mm | § 4.1.4.2.1 |
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| Concrete stress−2·m/(xII·z)compression negative | σc = -9.55 N/mm² | |
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| Bar stressm/(as·(d − xII/3)) | σs = 189.5 N/mm² | |
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Calculation: Check 1 — bar stress under the quasi-permanent load, top bars along x (supports, corners)| Step | Value | Ref. |
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| Bar stress against the crack limit, top bars along x (supports, corners)σs/fyk | η = 0.366 · Pass37 % of the capacity used | Table 17 |
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Calculation: Check 2 — bar stress under the quasi-permanent load, top bars along y (supports, corners)| Step | Value | Ref. |
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| Bar stress against the crack limit, top bars along y (supports, corners)σs/fyk | η = 0.379 · Pass38 % of the capacity used | Table 17 |
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Calculation: Deflection| Step | Value | Ref. |
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| Plate stiffnessEcm·h³/(12·(1 − ν²)) | D = 64,027 kNm | |
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| Elastic deflection, uncrackedelastic plate under qlargest at x = 15.20 m, y = 3.20 m | wc = 1.14 mm | |
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| Long-term deflection, uncrackedwc·(1 + φ) | wcφ = 3.68 mm | § 4.4.3.2.4 (103) |
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Calculation: Check 3 — deflection| Step | Value | Ref. |
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| Deflection against the admissible valuew/wadm | η = 0.153 · Pass15 % of the capacity used | § 4.4.3.2 |
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Calculation: Bar options| Step | Value | Ref. |
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| Cracking moment per metrekt·fctm·h²/6 | mcr = 36.2 kNm/m | § 4.4.1.3 |
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| Largest spacing allowedmin(1.2·h ; 300 mm) | smax = 300 mm | § 5.5.3.1 |
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Calculation: Bottom bars along x — chosen zone by zone| Step | Value | Ref. |
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| Zones with these barsof 216 zones of 1.02 × 1.03 m — Ø10@200: 216 | nz = 216 | |
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| Steel mass of this layerwithout laps and anchorages | G = 703 kg | |
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| Bending in every zone, bottom bars along xmax(md/mRd) | η = 0.966 · Pass97 % of the capacity used | § 4.3.2.6 |
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Calculation: Bottom bars along y — chosen zone by zone| Step | Value | Ref. |
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| Zones with these barsof 216 zones of 1.02 × 1.03 m — Ø10@200: 214, Ø12@200: 2 | nz = 216 | |
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| Steel mass of this layerwithout laps and anchorages | G = 706 kg | |
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| Bending in every zone, bottom bars along ymax(md/mRd) | η = 0.944 · Pass94 % of the capacity used | § 4.3.2.6 |
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Calculation: Top bars along x — chosen zone by zone| Step | Value | Ref. |
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| Zones with these barsof 216 zones of 1.02 × 1.03 m — Ø10@200: 129, Ø12@150: 8, Ø14@150: 22 | nz = 159 | |
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| Steel mass of this layerwithout laps and anchorages | G = 657 kg | |
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| Bending in every zone, top bars along xmax(md/mRd) | η = 0.997 · Pass100 % of the capacity used | § 4.3.2.6 |
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Calculation: Top bars along y — chosen zone by zone| Step | Value | Ref. |
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| Zones with these barsof 216 zones of 1.02 × 1.03 m — Ø10@200: 128, Ø12@150: 7, Ø14@150: 24 | nz = 159 | |
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| Steel mass of this layerwithout laps and anchorages | G = 665 kg | |
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| Bending in every zone, top bars along ymax(md/mRd) | η = 0.951 · Pass95 % of the capacity used | § 4.3.2.6 |
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| Total steel mass of the panel12.0 kg/m², without laps and anchorages | ΣG = 2,732 kg | |
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Calculation: Deflection with the chosen bars| Step | Value | Ref. |
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| Long-term deflection, uncracked | wcφ = 3.68 mm | § 4.4.3.2.4 (103) |
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| Deflection against the admissible valuew/wadm | η = 0.153 · Pass15 % of the capacity used | § 4.4.3.2 |
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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 are the moments over the columns averaged?
The elastic plate has sharp peaks at the column faces. The mean across the support strip bs keeps the total moment, is admissible with ductile reinforcement (4.1.4.2), and gives the msd of the punching check. Peak values are the safe-side option.
What does the warning on ψ mean?
Below ψ = 0.020 the deformation capacity is limited. Clause 4.3.6.1.2 then points to a larger column, a thicker slab or punching reinforcement meeting equation (67).
Can I print the calculation?
The full calculation is shown on screen, free and without an account. A print-ready A4 calculation note is part of the Basic plan.
Related
Norm: SIA 262:2025 · Page updated: 24 October 2026