Stress area: 156.67 mm² · Proof load: 35,251 N · Clamp load (75%): 26,438 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 84.6 | 62.4 | 748.8 | 862.7 |
| Oiled | 0.15 | 63.5 | 46.8 | 562.0 | 647.5 |
| Zinc Plated | 0.18 | 76.1 | 56.1 | 673.5 | 776.0 |
| Waxed | 0.1 | 42.3 | 31.2 | 374.4 | 431.3 |
| MoS₂ | 0.12 | 50.8 | 37.5 | 449.6 | 518.0 |
| Galvanized | 0.25 | 105.8 | 78.0 | 936.4 | 1078.9 |
Stress area: 167.25 mm² · Proof load: 37,631 N · Clamp load (75%): 28,223 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 90.3 | 66.6 | 799.2 | 920.8 |
| Oiled | 0.15 | 67.7 | 49.9 | 599.2 | 690.4 |
| Zinc Plated | 0.18 | 81.3 | 60.0 | 719.6 | 829.0 |
| Waxed | 0.1 | 45.2 | 33.3 | 400.1 | 460.9 |
| MoS₂ | 0.12 | 54.2 | 40.0 | 479.7 | 552.7 |
| Galvanized | 0.25 | 112.9 | 83.3 | 999.2 | 1151.3 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 225 MPa × 156.67 mm² = 26,438 N
Step 2 — Torque (dry): T = 0.20 × 0.0160 m × 26,438 N = 84.6 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