Stress area: 20.12 mm² · Proof load: 11,670 N · Clamp load (75%): 8,752 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 10.5 | 7.7 | 92.9 | 107.1 |
| Oiled | 0.15 | 7.9 | 5.8 | 69.9 | 80.6 |
| Zinc Plated | 0.18 | 9.5 | 7.0 | 84.1 | 96.9 |
| Waxed | 0.1 | 5.3 | 3.9 | 46.9 | 54.0 |
| MoS₂ | 0.12 | 6.3 | 4.6 | 55.8 | 64.2 |
| Galvanized | 0.25 | 13.1 | 9.7 | 115.9 | 133.6 |
Stress area: 22.03 mm² · Proof load: 12,777 N · Clamp load (75%): 9,583 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 11.5 | 8.5 | 101.8 | 117.3 |
| Oiled | 0.15 | 8.6 | 6.3 | 76.1 | 87.7 |
| Zinc Plated | 0.18 | 10.3 | 7.6 | 91.2 | 105.0 |
| Waxed | 0.1 | 5.7 | 4.2 | 50.4 | 58.1 |
| MoS₂ | 0.12 | 6.9 | 5.1 | 61.1 | 70.4 |
| Galvanized | 0.25 | 14.4 | 10.6 | 127.5 | 146.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 20.12 mm² = 8,752 N
Step 2 — Torque (dry): T = 0.20 × 0.0060 m × 8,752 N = 10.5 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