Stress area: 8.78 mm² · Proof load: 1,975 N · Clamp load (75%): 1,482 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1.2 | 0.9 | 10.6 | 12.2 |
| Oiled | 0.15 | 0.9 | 0.7 | 8.0 | 9.2 |
| Zinc Plated | 0.18 | 1.1 | 0.8 | 9.7 | 11.2 |
| Waxed | 0.1 | 0.6 | 0.4 | 5.3 | 6.1 |
| MoS₂ | 0.12 | 0.7 | 0.5 | 6.2 | 7.1 |
| Galvanized | 0.25 | 1.5 | 1.1 | 13.3 | 15.3 |
Stress area: 9.79 mm² · Proof load: 2,203 N · Clamp load (75%): 1,652 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1.3 | 1.0 | 11.5 | 13.3 |
| Oiled | 0.15 | 1.0 | 0.7 | 8.9 | 10.2 |
| Zinc Plated | 0.18 | 1.2 | 0.9 | 10.6 | 12.2 |
| Waxed | 0.1 | 0.7 | 0.5 | 6.2 | 7.1 |
| MoS₂ | 0.12 | 0.8 | 0.6 | 7.1 | 8.2 |
| Galvanized | 0.25 | 1.7 | 1.3 | 15.0 | 17.3 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 8.78 mm² = 1,482 N
Step 2 — Torque (dry): T = 0.20 × 0.0040 m × 1,482 N = 1.2 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Non-critical assemblies, light-duty applications, general-purpose hardware where high strength is not required