Material properties, shared by every verification. The cross-section is not shared: SIA 262 works from the section as sized for each internal-force case, so it belongs to each verification and appears with it.
Compares several bar configurations of a reinforced concrete slab section, 1 m wide, side by side, to SIA 262:2025: bending resistance, shear without stirrups, cracking moment and minimum reinforcement, anchorage and lap lengths, stiffness and service stresses. Every step shows its formula and the clause it comes from.
For each configuration, in its own column of one table:
You enter the configurations in a table, one line each: diameter and spacing of the tension bars and of the compression-face bars, the two covers and the thickness. Then the concrete and steel properties, εc2d, the resistance factors, the bond conditions (5.2.5.3), where the tension bars lie in the pour, and the stress in lapped bars (5.2.6.6). Optional: md, vd, the crack requirement level and a service moment m.
You get one column per configuration, ending in a pass or fail, and a drawing of the section, strains and forces of the configuration you choose. With the Basic plan, it prints as an A4 calculation note.
Nine configurations side by side, from Ø10 to Ø30 at 150 mm on the tension face with Ø10 or Ø12 at 150 mm on the other face, in slabs 200 to 500 mm thick with covers of 30 to 78 mm, fck = 30 N/mm² and fyk = 500 N/mm², without design or service actions; configuration 4, Ø16 over Ø10 at 150 mm in a 500 mm slab, is drawn. These are the module's own results for its worked example, computed when this page was built.
| Input | Value | Ref. |
|---|---|---|
| Configurations to compare | [[10,150,10,150,60,60,200],[12,150,12,150,30,30,300],[14,150,10,150,60,60,500],[16,150,10,150,60,60,500],[18,150,10,150,78,78,500],[20,150,10,150,74,74,250],[22,150,10,150,40,40,500],[26,150,10,150,40,40,500],[30,150,10,150,40,40,500]] | |
| Configuration drawn in the figures | 4 — Ø16@150 / Ø10@150 | |
| Characteristic compressive strength fck | 30 N/mm² | § 3.1.2.2.2 |
| Ultimate compressive strain εc2d | 3.5 ‰ | § 4.2.1.5 |
| Mean tensile strength fctm | 2.9 N/mm² | § 3.1.2.2.4 |
| Modulus of elasticity Ecm | 30000 N/mm² | § 3.1.2.3.3 |
| Largest aggregate size Dmax | 32 mm | § 4.3.3.2.1 |
| Characteristic yield strength fyk | 500 N/mm² | § 3.2.2.2 |
| Modulus of elasticity Es | 205000 N/mm² | § 3.2.2.4 |
| Resistance factor for concrete γc | 1.5 | § 2.4.2.6 |
| Resistance factor for steel γs | 1.15 | § 2.4.2.6 |
| Duration factor ηt | 1.0 — both conditions of 4.2.1.3 met | § 4.2.1.3 |
| Bond conditions | From the position of the bars in the pour (5.2.5.3) | § 5.2.5.3 |
| Tension bars in the pour | At the bottom of the pour (span, positive moment) | § 5.2.5.3 |
| Stress in the lapped tension bars σsd | 1.0·fyd — plastic strains excluded, or at most half the bars lapped | § 5.2.6.6 |
| Tensile strength for cracking | Mean tensile strength (4.4.1.3) | § 4.4.1.3 |
| Crack requirement level | Normal | § 4.4.2.2.3 |
| Step | Value | Ref. |
|---|---|---|
| Factor for the brittleness of strong concrete(40/fck)^(1/3) ≤ 1 | ηfc = 1.000 | § 4.2.1.2 (26) |
| Design compressive strength of the concreteηfc·ηt·fck/γcacting over 0.85·x (Figure 12) | fcd = 20.0 N/mm² | § 2.4.2.3 (2) |
| Design yield strength of the steelfyk/γs | fyd = 434.8 N/mm² | § 2.4.2.5 (4) |
| Yield strain of the steelfyd/Es | εyd = 2.12 ‰ | |
| Limits of x/d for ductility0.35·435/fyd (redistribution without check) ; 0.5·435/fyd (to be avoided above) | x/d = 0.350 ; 0.500 | § 4.1.4.2.5 |
| Design shear stress limit0.3·√fck/γc | τcd = 1.10 N/mm² | § 2.4.2.4 (3) |
| Aggregate factor48/(16 + Dmax·min(1 ; (60/fck)²)) ≥ 1.2 | kg = 1.200 | § 4.3.3.2.1 (37) |
| Tensile strength for crackingtimes kt = 1/(1 + 0.5·t), t = h/3 in m, for each thickness (100) | fctm = 2.90 N/mm² | § 4.4.1.3 (99) |
| Modular ratioEs/Ecm | αe = 6.83 |
| Step | 1Ø10@150Ø10@150h = 200 mm | 2Ø12@150Ø12@150h = 300 mm | 3Ø14@150Ø10@150h = 500 mm | 4Ø16@150Ø10@150h = 500 mm | 5Ø18@150Ø10@150h = 500 mm | 6Ø20@150Ø10@150h = 250 mm | 7Ø22@150Ø10@150h = 500 mm | 8Ø26@150Ø10@150h = 500 mm | 9Ø30@150Ø10@150h = 500 mm | Ref. |
|---|---|---|---|---|---|---|---|---|---|---|
| Reinforcement and section | ||||||||||
| Tension bars, diameter Øs mm | 10 | 12 | 14 | 16 | 18 | 20 | 22 | 26 | 30 | |
| Tension bars, spacing ss mm | 150 | 150 | 150 | 150 | 150 | 150 | 150 | 150 | 150 | |
| Compression-face bars, diameter Ø′s mm | 10 | 12 | 10 | 10 | 10 | 10 | 10 | 10 | 10 | |
| Compression-face bars, spacing s′s mm | 150 | 150 | 150 | 150 | 150 | 150 | 150 | 150 | 150 | |
| Cover, tension face c mm | 60 | 30 | 60 | 60 | 78 | 74 | 40 | 40 | 40 | |
| Cover, compression face c′ mm | 60 | 30 | 60 | 60 | 78 | 74 | 40 | 40 | 40 | |
| Thickness of the slab h mm | 200 | 300 | 500 | 500 | 500 | 250 | 500 | 500 | 500 | |
| Effective depth d mmh − c − Øs/2 | 135 | 264 | 433 | 432 | 413 | 166 | 449 | 447 | 445 | |
| Depth of the compression-face bars d′ mmc′ + Ø′s/2 | 65 | 36 | 65 | 65 | 83 | 79 | 45 | 45 | 45 | |
| Bars per metre n 1/m1000/ss | 6.67 | 6.67 | 6.67 | 6.67 | 6.67 | 6.67 | 6.67 | 6.67 | 6.67 | |
| Steel area, tension bars as mm²/mπ·Øs²/4 · 1000/ss | 524 | 754 | 1,026 | 1,340 | 1,696 | 2,094 | 2,534 | 3,540 | 4,712 | |
| Steel area, compression-face bars a′s mm²/mπ·Ø′s²/4 · 1000/s′s | 524 | 754 | 524 | 524 | 524 | 524 | 524 | 524 | 524 | |
| Reinforcement ratio, tension bars ρ %as/(b·d), b = 1000 mm | 0.388 | 0.286 | 0.237 | 0.310 | 0.411 | 1.262 | 0.564 | 0.792 | 1.059 | |
| Reinforcement ratio, compression-face bars ρ′ %a′s/(b·d) | 0.388 | 0.286 | 0.121 | 0.121 | 0.127 | 0.315 | 0.117 | 0.117 | 0.118 | |
| Bending resistance — ultimate limit state | ||||||||||
| Depth of the compression zone x mmequilibrium: fcd·b·0.85·x + a′s·σ′sd = as·σsd, with εc2d at the compressed face | 26.8 | 28.2 | 39.6 | 44.5 | 54.8 | 60.4 | 59.9 | 81.3 | 108.2 | § 4.2.1.5 |
| Relative depth of the compression zone x/d | 0.198 | 0.107 | 0.092 | 0.103 | 0.133 | 0.364 | 0.133 | 0.182 | 0.243 | |
| Strain of the tension bars εs ‰εc2d·(d − x)/x | 14.14 | 29.32 | 34.73 | 30.49 | 22.89 | 6.12 | 22.72 | 15.75 | 10.89 | |
| Stress of the tension bars σsd N/mm²Es·εs ≤ fyd | 435 | 435 | 435 | 435 | 435 | 435 | 435 | 435 | 435 | |
| Strain of the compression-face bars ε′s ‰εc2d·(x − d′)/x; negative: the bars are in tension | -4.99 | -0.98 | -2.24 | -1.61 | -1.80 | -1.08 | 0.87 | 1.56 | 2.04 | |
| Stress of the compression-face bars σ′sd N/mm²Es·ε′s, |σ′sd| ≤ fyd; compression positive | -435 | -200 | -435 | -331 | -370 | -221 | 179 | 320 | 419 | |
| Lever arm of the internal forces z mmmRd/(as·σsd) | 177 | 263 | 441 | 427 | 405 | 147 | 422 | 411 | 399 | |
| Bending resistance mRd kNm/mfcd·b·0.85·x·(d − 0.85·x/2) + a′s·σ′sd·(d − d′) | 40.3 | 86.2 | 196.6 | 248.7 | 299.0 | 134.0 | 465.0 | 633.1 | 817.7 | § 4.3.2.1 |
| Bending resistance, tension bars alone mRd,0 kNm/mthe compression-face bars left out | 29.4 | 83.9 | 188.2 | 243.3 | 291.0 | 130.4 | 464.4 | 628.7 | 806.8 | |
| Resistance to the opposite moment m′Rd kNm/mthe compression-face bars in tension, the tension bars on the compressed side | 40.3 | 86.2 | 117.6 | 120.5 | 134.6 | 77.4 | 115.3 | 117.2 | 119.1 | |
| Tension bars yield at failure εyd/εsεs ≥ εyd: a ductile failure, the steel yields before the concrete crushes | 0.15Pass | 0.07Pass | 0.06Pass | 0.07Pass | 0.09Pass | 0.35Pass | 0.09Pass | 0.13Pass | 0.19Pass | |
| Ductility for redistribution without a check (x/d)/limx/d ≤ 0.35·435/fyd; above, redistribute only with a check of the rotation capacity | 0.57met | 0.30met | 0.26met | 0.29met | 0.38met | 1.04exceeded | 0.38met | 0.52met | 0.69met | § 4.1.4.2.5 |
| Ductility of the compression zone (x/d)/limx/d ≤ 0.5·435/fyd, to be avoided above as far as possible | 0.40met | 0.21met | 0.18met | 0.21met | 0.27met | 0.73met | 0.27met | 0.36met | 0.49met | § 4.1.4.2.6 |
| Shear without stirrups — ultimate limit state | ||||||||||
| Strain for the shear resistance εv ‰1.5·fyd/Es: md taken equal to mRd (41), the lowest vRd | 3.181 | 3.181 | 3.181 | 3.181 | 3.181 | 3.181 | 3.181 | 3.181 | 3.181 | § 4.3.3.2.3 (41) |
| Coefficient kd1/(1 + εv·d·kg) | 0.660 | 0.498 | 0.377 | 0.377 | 0.388 | 0.612 | 0.368 | 0.369 | 0.371 | § 4.3.3.2.1 (36) |
| Shear resistance per metre vRd kN/mkd·τcd·dv, dv = d | 97.6 | 144.0 | 178.8 | 178.6 | 175.6 | 111.3 | 181.2 | 180.9 | 180.6 | § 4.3.3.2.1 (35) |
| Cracking moment and detailing | ||||||||||
| Size factor kt1/(1 + 0.5·h/3), h in m | 0.968 | 0.952 | 0.923 | 0.923 | 0.923 | 0.960 | 0.923 | 0.923 | 0.923 | § 4.4.1.3 (100) |
| Effective tensile strength fct,eff N/mm²kt·fctm | 2.81 | 2.76 | 2.68 | 2.68 | 2.68 | 2.78 | 2.68 | 2.68 | 2.68 | § 4.4.1.3 (99) |
| Cracking moment mcr kNm/mfct,eff·b·h²/6 | 18.7 | 41.4 | 111.5 | 111.5 | 111.5 | 29.0 | 111.5 | 111.5 | 111.5 | § 4.3.1.2 |
| Minimum reinforcement: no brittle failure at cracking mcr/mRdmRd ≥ mcr | 0.46Pass | 0.48Pass | 0.57Pass | 0.45Pass | 0.37Pass | 0.22Pass | 0.24Pass | 0.18Pass | 0.14Pass | § 4.3.1.2 |
| Largest bar spacing smax mmmin(1.2·h ; 300 mm) | 240 | 300 | 300 | 300 | 300 | 300 | 300 | 300 | 300 | § 5.5.3.1 |
| Spacing of the main bars in the most stressed zones ss/smaxss ≤ min(1.2·h ; 300 mm) | 0.63Pass | 0.50Pass | 0.50Pass | 0.50Pass | 0.50Pass | 0.50Pass | 0.50Pass | 0.50Pass | 0.50Pass | § 5.5.3.1 |
| Anchorage and laps | ||||||||||
| Bond, tension bars kcp1.0 good, 1.2 moderate (Figure 36b), 1.4 under bentonite | 1.0good | 1.0good | 1.0good | 1.0good | 1.0good | 1.0good | 1.0good | 1.0good | 1.0good | § 5.2.5.6 |
| Cover value for the anchorage, tension bars cd mmmin(0.5·(ss − Øs) ; c ; 3.75·Øs), side cover taken as c | 38 | 30 | 53 | 60 | 66 | 65 | 40 | 40 | 40 | § 5.2.5.2 (105) |
| Anchorage length, tension bars lbd mm50·kcp·Ø · (σsd/435)^1.5 · (25/fck)^0.5 · (Ø/20)^(1/3) · (1.5·Ø/cd)^0.5 ≥ 10·Ø, with σsd = fyd | 229 | 358 | 359 | 428 | 507 | 620 | 941 | 1,278 | 1,661 | § 5.2.5.6 (108) |
| Anchorage length in diameters lbd/Øs | 22.9 | 29.8 | 25.6 | 26.8 | 28.2 | 31.0 | 42.8 | 49.2 | 55.4 | |
| With an end hook or transverse compression lbd,hook mmlbd − 15·Øs ≥ 10·Øs | 100 | 178 | 149 | 188 | 237 | 320 | 611 | 888 | 1,211 | § 5.2.5.8 |
| Lap length, tension bars lsd mm1.2·lbd(fyd) ≥ 15·Øs, cs = ss − 2·Øs for touching bars (Figure 39a) | 275 | 429 | 430 | 518 | 655 | 808 | 1,129 | 1,534 | 1,994 | § 5.2.6.6 |
| Bond, compression-face bars k′cp | 1.0good | 1.0good | 1.2moderate | 1.2moderate | 1.2moderate | 1.0good | 1.2moderate | 1.2moderate | 1.2moderate | § 5.2.5.6 |
| Anchorage length, compression-face bars in tension l′bd mmeq. (108) with Ø′s, s′s, c′; for the opposite moment | 229 | 358 | 275 | 275 | 275 | 229 | 275 | 275 | 275 | § 5.2.5.6 (108) |
| Anchorage length, compression-face bars in compression l′bd,c mml′bd − 15·Ø′s ≥ 10·Ø′s, cover beyond the bar end > 5·Ø′s | 100 | 178 | 125 | 125 | 125 | 100 | 125 | 125 | 125 | § 5.2.5.7 |
| Lap length, compression-face bars in compression l′sd,c mm1.2·l′bd(fyd) ≥ 15·Ø′s | 275 | 429 | 330 | 330 | 330 | 275 | 330 | 330 | 330 | § 5.2.6.7 |
| Stiffness — serviceability | ||||||||||
| Centroid of the uncracked section yI mmfrom the compressed face, bars counted with αe | 100.0 | 150.0 | 251.0 | 251.7 | 252.2 | 126.4 | 254.5 | 256.6 | 258.9 | |
| Second moment, uncracked II 10⁶ mm⁴/m | 674 | 2,364 | 10,721 | 10,779 | 10,762 | 1,329 | 11,120 | 11,324 | 11,548 | |
| Neutral axis, cracked xII mmb·x²/2 + (αe − 1)·a′s·(x − d′) = αe·as·(d − x) | 31.3 | 46.4 | 71.0 | 79.8 | 86.8 | 57.2 | 107.1 | 123.2 | 138.5 | |
| Second moment, cracked III 10⁶ mm⁴/mb·x³/3 + αe·as·(d − x)² + (αe − 1)·a′s·(x − d′)² | 53 | 278 | 1,038 | 1,306 | 1,452 | 233 | 2,446 | 3,178 | 3,937 | |
| Flexural stiffness, uncracked Ecm·II kNm²/m | 20,224 | 70,930 | 321,634 | 323,363 | 322,872 | 39,858 | 333,603 | 339,711 | 346,441 | |
| Flexural stiffness, cracked Ecm·III kNm²/m | 1,583 | 8,332 | 31,152 | 39,187 | 43,546 | 7,005 | 73,367 | 95,337 | 118,120 | |
| Cracked over uncracked stiffness III/II | 0.078 | 0.117 | 0.097 | 0.121 | 0.135 | 0.176 | 0.220 | 0.281 | 0.341 | |
| Steel stress — crack limitation and yielding (Table 17) | ||||||||||
| Bar stress at cracking σs,r N/mm²mcr on the cracked section: αe·mcr·(d − xII)/III — imposed or restrained deformations, fct,eff reached | 251 | 222 | 266 | 206 | 171 | 92 | 107 | 78 | 59 | § 4.4.2.3.4 |
| Crack limitation at cracking (minimum reinforcement) σs,r/fykσs,r ≤ fyk (normal requirements) | 0.50Pass | 0.44Pass | 0.53Pass | 0.41Pass | 0.34Pass | 0.18Pass | 0.21Pass | 0.16Pass | 0.12Pass | Table 17 |
| Summary | ||||||||||
| Every check of this columnthe verifications above; the ductility limits are recommendations | Pass | Pass | Pass | Pass | Pass | Pass | Pass | Pass | Pass | |
Verified clause by clause against SIA 262:2025 and against independent calculations used on real projects, before release.
It selects the admissible bar stresses of Table 17. Normal: σs ≤ fyk. Increased and high: σs ≤ σs,adm of equation (102), and σs ≤ fyd − 80 N/mm² against yielding in service.
Where plastic strains cannot be excluded, unless at most half of the bars are lapped in one section, the lap is confined, or a plane stress state prevents cracking.
The full calculation is shown on screen, free and without an account. A print-ready A4 calculation note is part of the Basic plan.
Norm: SIA 262:2025 · Page updated: 24 October 2026