Stress area: 58.0 mm² · Proof load: 13,050 N · Clamp load (75%): 9,788 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 19.6 | 14.5 | 173.5 | 199.9 |
| Oiled | 0.15 | 14.7 | 10.8 | 130.1 | 149.9 |
| Zinc Plated | 0.18 | 17.6 | 13.0 | 155.8 | 179.5 |
| Waxed | 0.1 | 9.8 | 7.2 | 86.7 | 99.9 |
| MoS₂ | 0.12 | 11.7 | 8.6 | 103.6 | 119.3 |
| Galvanized | 0.25 | 24.5 | 18.1 | 216.8 | 249.8 |
Stress area: 61.2 mm² · Proof load: 13,770 N · Clamp load (75%): 10,328 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 20.7 | 15.3 | 183.2 | 211.1 |
| Oiled | 0.15 | 15.5 | 11.4 | 137.2 | 158.1 |
| Zinc Plated | 0.18 | 18.6 | 13.7 | 164.6 | 189.7 |
| Waxed | 0.1 | 10.3 | 7.6 | 91.2 | 105.0 |
| MoS₂ | 0.12 | 12.4 | 9.1 | 109.7 | 126.4 |
| Galvanized | 0.25 | 25.8 | 19.0 | 228.3 | 263.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 58.0 mm² = 9,788 N
Step 2 — Torque (dry): T = 0.20 × 0.0100 m × 9,788 N = 19.6 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Non-critical assemblies, light-duty applications, general-purpose hardware where high strength is not required