Stress area: 36.61 mm² · Proof load: 21,234 N · Clamp load (75%): 15,925 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 25.5 | 18.8 | 225.7 | 260.0 |
| Oiled | 0.15 | 19.1 | 14.1 | 169.0 | 194.8 |
| Zinc Plated | 0.18 | 22.9 | 16.9 | 202.7 | 233.5 |
| Waxed | 0.1 | 12.7 | 9.4 | 112.4 | 129.5 |
| MoS₂ | 0.12 | 15.3 | 11.3 | 135.4 | 156.0 |
| Galvanized | 0.25 | 31.9 | 23.5 | 282.3 | 325.3 |
Stress area: 39.17 mm² · Proof load: 22,719 N · Clamp load (75%): 17,039 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 27.3 | 20.1 | 241.6 | 278.4 |
| Oiled | 0.15 | 20.4 | 15.0 | 180.6 | 208.0 |
| Zinc Plated | 0.18 | 24.5 | 18.1 | 216.8 | 249.8 |
| Waxed | 0.1 | 13.6 | 10.0 | 120.4 | 138.7 |
| MoS₂ | 0.12 | 16.4 | 12.1 | 145.2 | 167.2 |
| Galvanized | 0.25 | 34.1 | 25.2 | 301.8 | 347.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 36.61 mm² = 15,925 N
Step 2 — Torque (dry): T = 0.20 × 0.0080 m × 15,925 N = 25.5 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