Stress area: 192.47 mm² · Proof load: 111,633 N · Clamp load (75%): 83,724 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 301.4 | 222.3 | 2667.6 | 3073.4 |
| Oiled | 0.15 | 226.1 | 166.8 | 2001.2 | 2305.6 |
| Zinc Plated | 0.18 | 271.3 | 200.1 | 2401.2 | 2766.5 |
| Waxed | 0.1 | 150.7 | 111.2 | 1333.8 | 1536.7 |
| MoS₂ | 0.12 | 180.8 | 133.4 | 1600.2 | 1843.7 |
| Galvanized | 0.25 | 376.8 | 277.9 | 3335.0 | 3842.3 |
Stress area: 216.23 mm² · Proof load: 125,413 N · Clamp load (75%): 94,060 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 338.6 | 249.7 | 2996.9 | 3452.8 |
| Oiled | 0.15 | 254.0 | 187.3 | 2248.1 | 2590.1 |
| Zinc Plated | 0.18 | 304.8 | 224.8 | 2697.7 | 3108.1 |
| Waxed | 0.1 | 169.3 | 124.9 | 1498.4 | 1726.4 |
| MoS₂ | 0.12 | 203.2 | 149.9 | 1798.5 | 2072.1 |
| Galvanized | 0.25 | 423.3 | 312.2 | 3746.5 | 4316.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 192.47 mm² = 83,724 N
Step 2 — Torque (dry): T = 0.20 × 0.0180 m × 83,724 N = 301.4 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