Stress area: 28.86 mm² · Proof load: 6,494 N · Clamp load (75%): 4,870 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 6.8 | 5.0 | 60.2 | 69.3 |
| Oiled | 0.15 | 5.1 | 3.8 | 45.1 | 52.0 |
| Zinc Plated | 0.18 | 6.1 | 4.5 | 54.0 | 62.2 |
| Waxed | 0.1 | 3.4 | 2.5 | 30.1 | 34.7 |
| MoS₂ | 0.12 | 4.1 | 3.0 | 36.3 | 41.8 |
| Galvanized | 0.25 | 8.5 | 6.3 | 75.2 | 86.7 |
Stress area: 31.23 mm² · Proof load: 7,027 N · Clamp load (75%): 5,270 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 7.4 | 5.5 | 65.5 | 75.5 |
| Oiled | 0.15 | 5.5 | 4.1 | 48.7 | 56.1 |
| Zinc Plated | 0.18 | 6.6 | 4.9 | 58.4 | 67.3 |
| Waxed | 0.1 | 3.7 | 2.7 | 32.7 | 37.7 |
| MoS₂ | 0.12 | 4.4 | 3.2 | 38.9 | 44.9 |
| Galvanized | 0.25 | 9.2 | 6.8 | 81.4 | 93.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 28.86 mm² = 4,870 N
Step 2 — Torque (dry): T = 0.20 × 0.0070 m × 4,870 N = 6.8 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