Stress area: 84.27 mm² · Proof load: 18,961 N · Clamp load (75%): 14,221 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 34.1 | 25.2 | 301.8 | 347.7 |
| Oiled | 0.15 | 25.6 | 18.9 | 226.6 | 261.0 |
| Zinc Plated | 0.18 | 30.7 | 22.6 | 271.7 | 313.1 |
| Waxed | 0.1 | 17.1 | 12.6 | 151.3 | 174.4 |
| MoS₂ | 0.12 | 20.5 | 15.1 | 181.4 | 209.0 |
| Galvanized | 0.25 | 42.7 | 31.5 | 377.9 | 435.4 |
Stress area: 92.07 mm² · Proof load: 20,716 N · Clamp load (75%): 15,537 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 37.3 | 27.5 | 330.1 | 380.4 |
| Oiled | 0.15 | 28.0 | 20.7 | 247.8 | 285.5 |
| Zinc Plated | 0.18 | 33.6 | 24.8 | 297.4 | 342.6 |
| Waxed | 0.1 | 18.6 | 13.7 | 164.6 | 189.7 |
| MoS₂ | 0.12 | 22.4 | 16.5 | 198.3 | 228.4 |
| Galvanized | 0.25 | 46.6 | 34.4 | 412.4 | 475.2 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 84.27 mm² = 14,221 N
Step 2 — Torque (dry): T = 0.20 × 0.0120 m × 14,221 N = 34.1 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Non-critical assemblies, light-duty applications, general-purpose hardware where high strength is not required