Stress area: 28.86 mm² · Proof load: 16,739 N · Clamp load (75%): 12,554 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 17.6 | 13.0 | 155.8 | 179.5 |
| Oiled | 0.15 | 13.2 | 9.7 | 116.8 | 134.6 |
| Zinc Plated | 0.18 | 15.8 | 11.7 | 139.8 | 161.1 |
| Waxed | 0.1 | 8.8 | 6.5 | 77.9 | 89.7 |
| MoS₂ | 0.12 | 10.5 | 7.7 | 92.9 | 107.1 |
| Galvanized | 0.25 | 22.0 | 16.2 | 194.7 | 224.3 |
Stress area: 31.23 mm² · Proof load: 18,113 N · Clamp load (75%): 13,585 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 19.0 | 14.0 | 168.2 | 193.7 |
| Oiled | 0.15 | 14.3 | 10.5 | 126.6 | 145.8 |
| Zinc Plated | 0.18 | 17.1 | 12.6 | 151.3 | 174.4 |
| Waxed | 0.1 | 9.5 | 7.0 | 84.1 | 96.9 |
| MoS₂ | 0.12 | 11.4 | 8.4 | 100.9 | 116.2 |
| Galvanized | 0.25 | 23.8 | 17.6 | 210.6 | 242.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 28.86 mm² = 12,554 N
Step 2 — Torque (dry): T = 0.20 × 0.0070 m × 12,554 N = 17.6 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