Stress area: 816.72 mm² · Proof load: 473,698 N · Clamp load (75%): 355,273 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2558.0 | 1886.7 | 22640.2 | 26084.4 |
| Oiled | 0.15 | 1918.5 | 1415.0 | 16980.2 | 19563.3 |
| Zinc Plated | 0.18 | 2302.2 | 1698.0 | 20376.2 | 23476.0 |
| Waxed | 0.1 | 1279.0 | 943.3 | 11320.1 | 13042.2 |
| MoS₂ | 0.12 | 1534.8 | 1132.0 | 13584.1 | 15650.7 |
| Galvanized | 0.25 | 3197.5 | 2358.4 | 28300.3 | 32605.5 |
Stress area: 864.95 mm² · Proof load: 501,671 N · Clamp load (75%): 376,253 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2709.0 | 1998.1 | 23976.7 | 27624.2 |
| Oiled | 0.15 | 2031.8 | 1498.6 | 17983.0 | 20718.7 |
| Zinc Plated | 0.18 | 2438.1 | 1798.2 | 21579.0 | 24861.8 |
| Waxed | 0.1 | 1354.5 | 999.0 | 11988.3 | 13812.1 |
| MoS₂ | 0.12 | 1625.4 | 1198.8 | 14386.0 | 16574.5 |
| Galvanized | 0.25 | 3386.3 | 2497.6 | 29971.3 | 34530.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 816.72 mm² = 355,273 N
Step 2 — Torque (dry): T = 0.20 × 0.0360 m × 355,273 N = 2558.0 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