Tightening torque and clamp-load preload from T = K·F·d — real ISO 8.8/10.9/12.9, ASTM A325/A490 and SAE proof strengths, a nut-factor table, dual kN/lbf output, the NBR 8800 · AISC minimum pretension, live bolt shear/tension from the connection engine, free CSV/PDF export, a shareable link and one-click hand-off to the 3D editor. No login.
Tightening torque
610 N·m
K±25%: 457–762 N·m
Bolt preload (clamp)
152.4 kN
34,257 lbf
Tensile stress area Aₛ
244.8 mm²
proof 203.2 kN
Proof / yield load
203.2 kN
yield 220.3 kN
How this torque is built — T = K · F · d
Aₛ = 0.7854·(d − 0.9382·P)² = 244.8 mm² (P = 2.5 mm) · engine table Aₛ = 245 mm²
Fₚ (proof) = Aₛ·Sp = 244.8·830 = 203.2 kN
F (preload) = 75%·Fₚ = 152.4 kN = 34,257 lbf
T = K·F·d = 0.20 · 152.4 kN · 20 mm = 610 N·m = 450 lbf·ft
Nut-factor scatter is real — ±25 % on K (Bickford)
Same preload, torque range: 457 N·m … 762 N·mK = 0.20 → 0.150…0.250
Same torque, preload actually installed: 121.9 kN … 203.2 kNa high real K under-tensions the joint
Bolt shear + tension capacity — live from the CalcSteel connection engine
These come straight from engine/connections/boltData — the same NBR 8800:2024 nominal strengths the 3D-editor connection design uses. Torque installs the clamp; this is what the bolt can carry. Single bolt, one shear plane.
Fnv (NBR)
450 MPa
Fnt
750 MPa
φRn — shear
71.6 kN
φRn — tension
119.3 kN
fub = 1000 MPa · Ab = 314 mm² · Aₛ = 245 mm² · φ = 0.65
Structural joints — minimum pretension Tb (NBR 8800 · AISC/RCSC)
Slip-critical and pretensioned connections do not aim for a % of proof load — the code fixes a minimum bolt tension Tb = 0.70·Fu·Aₛ per diameter. Below is that value for the two structural grades at M20, plus the K·Tb·d wrench torque (turn-of-nut and DTI are the code-preferred methods — torque is calibration-only).
ASTM A325 (≈ ISO 8.8)
Tb = 142.2 kN = 31,974 lbf
torque ≈ 569 N·m = 420 lbf·ft
ASTM A490 (≈ ISO 10.9)
Tb = 178.2 kN = 40,063 lbf
torque ≈ 713 N·m = 526 lbf·ft
Bolt torque chart — ISO 10.9 · Plain / as-received (dry) · 75% proof
| Size | Aₛ (mm²) | Preload F | Torque (N·m) | Torque (lbf·ft) |
|---|---|---|---|---|
| 20.1 | 12.5 kN | 15 | 11 | |
| 36.6 | 22.8 kN | 36.5 | 27 | |
| 58 | 36.1 kN | 72.2 | 53 | |
| 84.3 | 52.5 kN | 126 | 93 | |
| 115 | 71.9 kN | 201 | 148 | |
| 157 | 97.5 kN | 312 | 230 | |
| 192 | 119.8 kN | 431 | 318 | |
| 245 | 152.4 kN | 610 | 450 | |
| 303 | 188.9 kN | 831 | 613 | |
| 353 | 219.4 kN | 1,053 | 777 | |
| 459 | 286 kN | 1,544 | 1,139 | |
| 561 | 349 kN | 2,094 | 1,544 | |
| 817 | 508.4 kN | 3,661 | 2,700 |
Nut factors are typical published values — real scatter is ±25 %. For critical joints, calibrate K on your actual fastener/lubricant. Torque values are guidance, not a substitute for a qualified design.
A bolt torque calculator converts the tightening torque you apply with a wrench into the preload (the axial clamp force) it creates in the bolt — and back again. That preload is the whole point of a bolted joint: it is the tension locked into the shank that squeezes the connected parts together, keeps the joint from separating or slipping, and stops the bolt from working loose under vibration and fatigue. Torque itself is only the means of installing that preload; it is never the design objective.
The relationship both directions rest on is the short-form torque equation (also called the Motosh or nut-factor equation):
T = K · F · d
This calculator does the full chain for you. Pick the diameter (metric M or imperial UNC), the strength class, the surface condition, and the fraction of proof load you want to reach; it computes the tensile stress area, the proof and yield loads, the target preload, and the torque — all pre-solved the moment the page loads, with the answer shown in both kN and lbf for preload and both N·m and lbf·ft for torque. Unlike a generic mechanical torque app, it also carries the real proof strengths of every common bolt class and the structural minimum pretension Tb that steel design codes require for slip-critical and pretensioned connections.
The full torque balance of a threaded fastener has three parts — the torque that stretches the bolt through the thread helix, the torque lost to friction on the thread flanks, and the torque lost to friction under the turning nut face:
T = F · [ (P / 2π) + (μt · rt / cosα) + μn · rn ]
where P is the thread pitch, μt and μn are the thread and under-head friction coefficients, rt and rn the effective thread and bearing radii, and α the thread half-angle. Because all of those geometric and friction terms scale with the diameter, the whole bracket collapses to a single dimensionless nut factor K times the diameter d, which is why the short form T = K·F·d works so well in practice. The catch is that K is not a friction coefficient — a "K = 0.20" joint does not have μ = 0.20. K is an empirical property of the whole fastener system: bolt, nut, washer, plating and lubricant together.
Tensile stress area Aₛ. The bolt does not resist tension on its nominal area — the threads reduce it. Design uses the tensile stress area, the area of a hypothetical round bar with a diameter halfway between the pitch and minor thread diameters:
metric: Aₛ = 0.7854 · (d − 0.9382·P)² (mm², P = pitch)
imperial: Aₛ = 0.7854 · (d − 0.9743/n)² (in², n = threads per inch)
For an M20 coarse bolt (P = 2.5 mm) this gives Aₛ = 244.8 mm² — matching the 245 mm² published in every fastener table. Every strength quantity below is Aₛ times a stress.
From stress to preload. Each class has a proof stress Sp (the stress the bolt can carry with no measurable permanent set). The proof load is Fp = Aₛ·Sp, and the target preload is a chosen fraction of it — commonly 75 % for reusable joints and up to 90 % for permanent ones (closer to the yield load Aₛ·Re). Enter that fraction and the calculator returns F, then T = K·F·d.
The number stamped on a bolt head is not decoration — it encodes the strength. This calculator carries the real, standardised values, not one generic curve:
ISO 898-1 property classes (metric). The two-part mark "x.y" means ultimate tensile Rm ≈ x·100 MPa and yield ≈ x·y·10 MPa:
| Class | Proof Sp (MPa) | Yield Re (MPa) | Tensile Rm (MPa) | Typical use |
|---|---|---|---|---|
| 4.6 | 225 | 240 | 400 | mild-steel general |
| 5.8 | 380 | 420 | 520 | medium-duty |
| 8.8 | 580 | 640 | 800 | structural & machine standard |
| 10.9 | 830 | 900 | 1040 | high-strength |
| 12.9 | 970 | 1080 | 1220 | alloy, highest grade |
ASTM F3125 (the standard that absorbed the old A325 and A490) — the workhorses of North-American steel construction:
| Grade | Proof (MPa) | Tensile Fu (MPa) | ≈ ISO |
|---|---|---|---|
| A325 | 585 | 830 (120 ksi) | 8.8 |
| A490 | 825 | 1040 (150 ksi) | 10.9 |
(For imperial A325 the tensile strength drops from 120 ksi to 105 ksi above 1-in diameter; the calculator applies that reduction automatically.)
SAE J429 (imperial, common in mechanical and automotive work): Grade 2 (Sp 379 MPa / 55 ksi), Grade 5 (585 MPa / 85 ksi ≈ ISO 8.8), Grade 8 (827 MPa / 120 ksi ≈ ISO 10.9). Grade markings are the radial lines on the head — no lines for Gr 2, three lines for Gr 5, six for Gr 8.
Switch class in the tool and every downstream number — proof load, preload, torque and the whole torque chart — updates instantly.
If torque control gets a bad reputation, K is the reason. Because T = K·F·d, any error in K passes straight through to the preload: two joints torqued identically but with K differing by 25 % end up with preloads differing by 25 %. And K really does vary that much — it is set almost entirely by friction and lubrication, not by how hard you pull.
Typical published nut factors (Bickford, Introduction to the Design and Behavior of Bolted Joints; Fastenal / Machinery's Handbook):
| Surface / lubrication | Nut factor K |
|---|---|
| Plain / as-received steel, dry | 0.20 |
| Zinc-plated (electroplated) | 0.22 |
| Hot-dip galvanized, dry | 0.25 |
| Galvanized + wax or lube | 0.12 |
| Lightly oiled | 0.18 |
| Waxed · MoS₂ · PTFE anti-seize | 0.10 |
Two practical consequences:
For anything critical, calibrate K on your own fastener–lubricant combination (a bolt-tension calibrator or a load cell in a Skidmore-Wilhelm device). The table gives a defensible starting point, not a certified value — which is also why steel codes prefer preload-verifying methods over torque, as the next section explains.
This is where a structural bolt torque calculator parts ways with a mechanical one. In machine design you pick a preload as a fraction of proof load. In steel construction, slip-critical and pretensioned connections have a code-mandated minimum bolt pretension Tb that must be installed regardless — it is what develops the friction (faying-surface slip resistance) that the joint is designed on.
Both NBR 8800 (Tabela 20) and the AISC 360 / RCSC specification set the same value: 70 % of the minimum tensile strength,
Tb = 0.70 · Fu · Aₛ
The calculator computes Tb for the chosen diameter for both structural grades and shows the wrench torque K·Tb·d needed to reach it. A few benchmark values it reproduces exactly:
| Bolt | Tb — A325 | Tb — A490 |
|---|---|---|
| M16 | 91 kN | 114 kN |
| M20 | 142 kN | 178 kN |
| M24 | 205 kN | 257 kN |
| M30 | 326 kN | 408 kN |
| 3/4 in | 28 kip | 35 kip |
| 7/8 in | 39 kip | 49 kip |
| 1 in | 51 kip | 64 kip |
These match NBR 8800 Tabela 20 and AISC/RCSC Table 7.1 to the kilonewton.
Important: for structural work, torque is a last-resort installation method. RCSC ranks four: turn-of-the-nut, direct-tension-indicator (DTI) washers, tension-control (twist-off) bolts, and calibrated wrench. The calibrated-wrench method is the only one that uses torque, and it requires daily calibration on a bolt-tension device — with the torque set 5 % above K·Tb·d to cover scatter. Use the torque here to estimate and to sanity-check; verify the actual tension with turn-of-nut or DTIs on the real joint.
Worked example
Given
1. Tensile stress area
Aₛ = 0.7854·(20 − 0.9382·2.5)²
244.8 mm² (table 245)
2. Proof load
Fp = Aₛ·Sp = 244.8 × 830
203.2 kN
3. Target preload
F = 0.75 × 203.2
152.4 kN = 34,257 lbf
4. Tightening torque
T = K·F·d = 0.20 × 152.4 kN × 0.020 m
609.5 N·m = 449.6 lbf·ft
5. Structural cross-check (A490, NBR 8800 · AISC)
Tb = 0.70·Fu·Aₛ = 0.70 × 1040 × 244.8
178.2 kN (min pretension) → torque ≈ 713 N·m
Result
T = 610 N·m (450 lbf·ft) for 152 kN preload · code min pretension Tb = 142 kN (A325) / 178 kN (A490)
T = K·F·d, where T is tightening torque, K is the nut factor (torque coefficient, ~0.10–0.25 depending on lubrication and finish), F is the target preload (bolt tension), and d is the nominal bolt diameter. It is the short form of the full thread-friction torque balance; because every geometric and friction term scales with diameter, they collapse into the single factor K.
Yes — this page builds a live bolt torque chart for the class and surface you select, listing tightening torque (N·m and lbf·ft), preload and tensile stress area for the whole size series (M6–M36 or 1/2 in–1-1/2 in). Change the grade, lubrication or preload % and the entire chart updates. Click any row to load that size into the sketch and KPIs.
About 610 N·m (450 lbf·ft) for a dry (K = 0.20) bolt tightened to 75 % of proof load — that installs roughly 152 kN of preload. Lubricated to K = 0.12 the same 152 kN needs only about 365 N·m. Grade 8.8 needs proportionally less (its proof stress is 580 vs 830 MPa). Use the calculator to match your exact class, finish and preload target.
K is a dimensionless coefficient that lumps thread friction, under-head friction and the thread lead into one number in T = K·F·d. It is set mainly by finish and lubrication: ~0.20 dry plain steel, 0.22 zinc-plated, 0.25 hot-dip galvanized dry, 0.10–0.12 waxed/MoS₂/PTFE. It is NOT a friction coefficient. For critical joints, calibrate K on your actual bolt/lubricant with a bolt-tension device rather than trusting a table.
Because most of the torque is spent overcoming friction, not stretching the bolt. Lower friction (lubrication) means more of the torque turns into preload, so you need much less torque for the same tension — roughly half, going from galvanized dry (K ≈ 0.25) to waxed (K ≈ 0.12). Torque a lubricated bolt to the dry value and you over-tension it and can snap it.
Use ~75 % of proof load for joints that will be disassembled and reused, and up to ~90 % (near yield) for permanent, gasketed or fatigue-critical joints where maximum clamp is wanted. Higher preload improves fatigue and loosening resistance but leaves less margin before yield. This tool lets you set any fraction from 30 % to 95 %.
Structural slip-critical and pretensioned joints do not target a % of proof load — the code fixes a minimum bolt pretension Tb = 0.70·Fu·As (NBR 8800 Tabela 20 and AISC/RCSC Table 7.1). For example M20 A325 needs 142 kN and M20 A490 needs 178 kN. This page shows Tb and the torque to reach it for both grades at your diameter.
Only as the "calibrated wrench" method, and only with daily calibration on a bolt-tension calibrator, torque set ~5% above K·Tb·d. AISC/RCSC prefer turn-of-the-nut, direct-tension-indicator (DTI) washers, or tension-control twist-off bolts, because they verify tension directly rather than inferring it from a scattered nut factor. Use the torque here to estimate and cross-check, not as the sole control.
The threads remove material, so a bolt in tension resists on the tensile stress area Aₛ = 0.7854·(d − 0.9382·P)² (metric) — the area of a bar sized between the pitch and minor thread diameters. For M20 that is 244.8 mm² vs 314 mm² nominal. All proof, yield and preload figures use Aₛ, which is why the calculator computes it first.
Yes. Preload is always shown in kN and lbf, and torque in N·m and lbf·ft, whichever thread system you pick. The SI ⇄ imperial toggle chooses which is primary; the other stays visible so a shop in either system can read it directly.
Yes, free and without login or watermark. Download a CSV that carries the single-bolt result strip (Aₛ, Fp, F, T, Tb for A325/A490) plus the whole size-series torque chart for your class, surface and preload %. Print → PDF bundles the dimensioned sketch and results into one page. And every input lives in the URL, so "Copy link" produces a permalink (?sys=metric&sz=M20&g=10.9&s=dry&pc=75) that rebuilds your exact bolt — a screenshot and the link together are fully shareable.
Two ways. The tool shows a live bolt shear + tension capacity card (Fnv/Fnt and φRn) sourced straight from the connection engine (engine/connections/boltData) — the same AISC 360 Table J3.2 / NBR 8800:2024 tables the 3D-editor uses, not a re-typed handbook. And "Open this bolt in the 3D editor" builds a real, prefilled base-plate connection (fixed-base column + base plate whose anchors already carry your diameter and grade), ready for the full NBR 8800 / AISC 360 connection check, combinations and PDF report.
Yes. A fine pitch removes less material, so the tensile stress area Aₛ is larger — for M20 it rises from 244.8 mm² (coarse, P = 2.5) to about 271.5 mm² (fine, P = 1.5), roughly +11 % more proof load and preload for the same stress, and proportionally more torque. Tick "fine thread" (metric sizes) to switch every downstream number and the whole chart to the fine-pitch area — a case single-curve calculators quietly ignore.
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