Stress area: 8.78 mm² · Proof load: 5,092 N · Clamp load (75%): 3,819 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3.1 | 2.3 | 27.4 | 31.6 |
| Oiled | 0.15 | 2.3 | 1.7 | 20.4 | 23.5 |
| Zinc Plated | 0.18 | 2.7 | 2.0 | 23.9 | 27.5 |
| Waxed | 0.1 | 1.5 | 1.1 | 13.3 | 15.3 |
| MoS₂ | 0.12 | 1.8 | 1.3 | 15.9 | 18.4 |
| Galvanized | 0.25 | 3.8 | 2.8 | 33.6 | 38.7 |
Stress area: 9.79 mm² · Proof load: 5,678 N · Clamp load (75%): 4,259 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3.4 | 2.5 | 30.1 | 34.7 |
| Oiled | 0.15 | 2.6 | 1.9 | 23.0 | 26.5 |
| Zinc Plated | 0.18 | 3.1 | 2.3 | 27.4 | 31.6 |
| Waxed | 0.1 | 1.7 | 1.3 | 15.0 | 17.3 |
| MoS₂ | 0.12 | 2.0 | 1.5 | 17.7 | 20.4 |
| Galvanized | 0.25 | 4.3 | 3.2 | 38.1 | 43.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 8.78 mm² = 3,819 N
Step 2 — Torque (dry): T = 0.20 × 0.0040 m × 3,819 N = 3.1 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Automotive engines, structural connections, high-strength machinery, flanged joints — the most common high-strength grade