Stress area: 303.4 mm² · Proof load: 175,972 N · Clamp load (75%): 131,979 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 580.7 | 428.3 | 5139.6 | 5921.5 |
| Oiled | 0.15 | 435.5 | 321.2 | 3854.5 | 4440.9 |
| Zinc Plated | 0.18 | 522.6 | 385.4 | 4625.4 | 5329.1 |
| Waxed | 0.1 | 290.4 | 214.2 | 2570.3 | 2961.3 |
| MoS₂ | 0.12 | 348.4 | 257.0 | 3083.6 | 3552.7 |
| Galvanized | 0.25 | 725.9 | 535.4 | 6424.8 | 7402.1 |
Stress area: 333.01 mm² · Proof load: 193,146 N · Clamp load (75%): 144,859 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 637.4 | 470.1 | 5641.5 | 6499.7 |
| Oiled | 0.15 | 478.0 | 352.6 | 4230.7 | 4874.3 |
| Zinc Plated | 0.18 | 573.6 | 423.1 | 5076.8 | 5849.1 |
| Waxed | 0.1 | 318.7 | 235.1 | 2820.7 | 3249.8 |
| MoS₂ | 0.12 | 382.4 | 282.0 | 3384.5 | 3899.4 |
| Galvanized | 0.25 | 796.7 | 587.6 | 7051.4 | 8124.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 303.4 mm² = 131,979 N
Step 2 — Torque (dry): T = 0.20 × 0.0220 m × 131,979 N = 580.7 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