Stress area: 58.0 mm² · Proof load: 33,640 N · Clamp load (75%): 25,230 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 50.5 | 37.2 | 447.0 | 515.0 |
| Oiled | 0.15 | 37.8 | 27.9 | 334.6 | 385.5 |
| Zinc Plated | 0.18 | 45.4 | 33.5 | 401.8 | 463.0 |
| Waxed | 0.1 | 25.2 | 18.6 | 223.0 | 257.0 |
| MoS₂ | 0.12 | 30.3 | 22.3 | 268.2 | 309.0 |
| Galvanized | 0.25 | 63.1 | 46.5 | 558.5 | 643.4 |
Stress area: 61.2 mm² · Proof load: 35,496 N · Clamp load (75%): 26,622 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 53.2 | 39.2 | 470.9 | 542.5 |
| Oiled | 0.15 | 39.9 | 29.4 | 353.1 | 406.9 |
| Zinc Plated | 0.18 | 47.9 | 35.3 | 424.0 | 488.4 |
| Waxed | 0.1 | 26.6 | 19.6 | 235.4 | 271.2 |
| MoS₂ | 0.12 | 31.9 | 23.5 | 282.3 | 325.3 |
| Galvanized | 0.25 | 66.6 | 49.1 | 589.5 | 679.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 58.0 mm² = 25,230 N
Step 2 — Torque (dry): T = 0.20 × 0.0100 m × 25,230 N = 50.5 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Automotive engines, structural connections, high-strength machinery, flanged joints — the most common high-strength grade