Stress area: 352.5 mm² · Proof load: 204,450 N · Clamp load (75%): 153,338 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 736.0 | 542.8 | 6514.2 | 7505.1 |
| Oiled | 0.15 | 552.0 | 407.1 | 4885.6 | 5628.9 |
| Zinc Plated | 0.18 | 662.4 | 488.6 | 5862.7 | 6754.6 |
| Waxed | 0.1 | 368.0 | 271.4 | 3257.1 | 3752.6 |
| MoS₂ | 0.12 | 441.6 | 325.7 | 3908.5 | 4503.1 |
| Galvanized | 0.25 | 920.0 | 678.6 | 8142.7 | 9381.4 |
Stress area: 384.42 mm² · Proof load: 222,964 N · Clamp load (75%): 167,223 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 802.7 | 592.0 | 7104.5 | 8185.3 |
| Oiled | 0.15 | 602.0 | 444.0 | 5328.2 | 6138.7 |
| Zinc Plated | 0.18 | 722.4 | 532.8 | 6393.8 | 7366.5 |
| Waxed | 0.1 | 401.3 | 296.0 | 3551.8 | 4092.1 |
| MoS₂ | 0.12 | 481.6 | 355.2 | 4262.5 | 4911.0 |
| Galvanized | 0.25 | 1003.3 | 740.0 | 8880.0 | 10230.9 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 352.5 mm² = 153,338 N
Step 2 — Torque (dry): T = 0.20 × 0.0240 m × 153,338 N = 736.0 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