Stress area: 14.18 mm² · Proof load: 3,190 N · Clamp load (75%): 2,393 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2.4 | 1.8 | 21.2 | 24.5 |
| Oiled | 0.15 | 1.8 | 1.3 | 15.9 | 18.4 |
| Zinc Plated | 0.18 | 2.2 | 1.6 | 19.5 | 22.4 |
| Waxed | 0.1 | 1.2 | 0.9 | 10.6 | 12.2 |
| MoS₂ | 0.12 | 1.4 | 1.0 | 12.4 | 14.3 |
| Galvanized | 0.25 | 3.0 | 2.2 | 26.6 | 30.6 |
Stress area: 16.13 mm² · Proof load: 3,629 N · Clamp load (75%): 2,722 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2.7 | 2.0 | 23.9 | 27.5 |
| Oiled | 0.15 | 2.0 | 1.5 | 17.7 | 20.4 |
| Zinc Plated | 0.18 | 2.4 | 1.8 | 21.2 | 24.5 |
| Waxed | 0.1 | 1.4 | 1.0 | 12.4 | 14.3 |
| MoS₂ | 0.12 | 1.6 | 1.2 | 14.2 | 16.3 |
| Galvanized | 0.25 | 3.4 | 2.5 | 30.1 | 34.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 14.18 mm² = 2,393 N
Step 2 — Torque (dry): T = 0.20 × 0.0050 m × 2,393 N = 2.4 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