Stress area: 84.27 mm² · Proof load: 48,877 N · Clamp load (75%): 36,657 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 88.0 | 64.9 | 778.9 | 897.4 |
| Oiled | 0.15 | 66.0 | 48.7 | 584.1 | 673.0 |
| Zinc Plated | 0.18 | 79.2 | 58.4 | 701.0 | 807.6 |
| Waxed | 0.1 | 44.0 | 32.5 | 389.4 | 448.7 |
| MoS₂ | 0.12 | 52.8 | 38.9 | 467.3 | 538.4 |
| Galvanized | 0.25 | 110.0 | 81.1 | 973.6 | 1121.7 |
Stress area: 92.07 mm² · Proof load: 53,401 N · Clamp load (75%): 40,050 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 96.1 | 70.9 | 850.6 | 980.0 |
| Oiled | 0.15 | 72.1 | 53.2 | 638.1 | 735.2 |
| Zinc Plated | 0.18 | 86.5 | 63.8 | 765.6 | 882.1 |
| Waxed | 0.1 | 48.1 | 35.5 | 425.7 | 490.5 |
| MoS₂ | 0.12 | 57.7 | 42.6 | 510.7 | 588.4 |
| Galvanized | 0.25 | 120.2 | 88.7 | 1063.9 | 1225.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 84.27 mm² = 36,657 N
Step 2 — Torque (dry): T = 0.20 × 0.0120 m × 36,657 N = 88.0 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