Stress area: 115.44 mm² · Proof load: 66,955 N · Clamp load (75%): 50,216 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 140.6 | 103.7 | 1244.4 | 1433.7 |
| Oiled | 0.15 | 105.5 | 77.8 | 933.8 | 1075.8 |
| Zinc Plated | 0.18 | 126.5 | 93.3 | 1119.6 | 1289.9 |
| Waxed | 0.1 | 70.3 | 51.9 | 622.2 | 716.9 |
| MoS₂ | 0.12 | 84.4 | 62.3 | 747.0 | 860.6 |
| Galvanized | 0.25 | 175.8 | 129.7 | 1556.0 | 1792.7 |
Stress area: 124.55 mm² · Proof load: 72,239 N · Clamp load (75%): 54,179 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 151.7 | 111.9 | 1342.7 | 1546.9 |
| Oiled | 0.15 | 113.8 | 83.9 | 1007.2 | 1160.4 |
| Zinc Plated | 0.18 | 136.5 | 100.7 | 1208.1 | 1391.9 |
| Waxed | 0.1 | 75.9 | 56.0 | 671.8 | 774.0 |
| MoS₂ | 0.12 | 91.0 | 67.1 | 805.4 | 927.9 |
| Galvanized | 0.25 | 189.6 | 139.8 | 1678.1 | 1933.4 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 115.44 mm² = 50,216 N
Step 2 — Torque (dry): T = 0.20 × 0.0140 m × 50,216 N = 140.6 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