Stress area: 459.41 mm² · Proof load: 266,458 N · Clamp load (75%): 199,843 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1079.2 | 796.0 | 9551.7 | 11004.8 |
| Oiled | 0.15 | 809.4 | 597.0 | 7163.8 | 8253.6 |
| Zinc Plated | 0.18 | 971.2 | 716.3 | 8595.8 | 9903.5 |
| Waxed | 0.1 | 539.6 | 398.0 | 4775.9 | 5502.4 |
| MoS₂ | 0.12 | 647.5 | 477.6 | 5730.9 | 6602.7 |
| Galvanized | 0.25 | 1348.9 | 994.9 | 11938.8 | 13755.0 |
Stress area: 496.18 mm² · Proof load: 287,784 N · Clamp load (75%): 215,838 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1165.5 | 859.6 | 10315.5 | 11884.8 |
| Oiled | 0.15 | 874.1 | 644.7 | 7736.4 | 8913.4 |
| Zinc Plated | 0.18 | 1049.0 | 773.7 | 9284.4 | 10696.9 |
| Waxed | 0.1 | 582.8 | 429.9 | 5158.2 | 5942.9 |
| MoS₂ | 0.12 | 699.3 | 515.8 | 6189.3 | 7130.9 |
| Galvanized | 0.25 | 1456.9 | 1074.6 | 12894.7 | 14856.3 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 459.41 mm² = 199,843 N
Step 2 — Torque (dry): T = 0.20 × 0.0270 m × 199,843 N = 1079.2 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