Stress area: 14.18 mm² · Proof load: 8,224 N · Clamp load (75%): 6,168 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 6.2 | 4.6 | 54.9 | 63.2 |
| Oiled | 0.15 | 4.6 | 3.4 | 40.7 | 46.9 |
| Zinc Plated | 0.18 | 5.6 | 4.1 | 49.6 | 57.1 |
| Waxed | 0.1 | 3.1 | 2.3 | 27.4 | 31.6 |
| MoS₂ | 0.12 | 3.7 | 2.7 | 32.7 | 37.7 |
| Galvanized | 0.25 | 7.7 | 5.7 | 68.2 | 78.5 |
Stress area: 16.13 mm² · Proof load: 9,355 N · Clamp load (75%): 7,017 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 7.0 | 5.2 | 62.0 | 71.4 |
| Oiled | 0.15 | 5.3 | 3.9 | 46.9 | 54.0 |
| Zinc Plated | 0.18 | 6.3 | 4.6 | 55.8 | 64.2 |
| Waxed | 0.1 | 3.5 | 2.6 | 31.0 | 35.7 |
| MoS₂ | 0.12 | 4.2 | 3.1 | 37.2 | 42.8 |
| Galvanized | 0.25 | 8.8 | 6.5 | 77.9 | 89.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 14.18 mm² = 6,168 N
Step 2 — Torque (dry): T = 0.20 × 0.0050 m × 6,168 N = 6.2 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