Stress area: 244.79 mm² · Proof load: 141,978 N · Clamp load (75%): 106,484 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 425.9 | 314.1 | 3769.5 | 4343.0 |
| Oiled | 0.15 | 319.5 | 235.7 | 2827.8 | 3258.0 |
| Zinc Plated | 0.18 | 383.3 | 282.7 | 3392.5 | 3908.6 |
| Waxed | 0.1 | 213.0 | 157.1 | 1885.2 | 2172.0 |
| MoS₂ | 0.12 | 255.6 | 188.5 | 2262.3 | 2606.4 |
| Galvanized | 0.25 | 532.4 | 392.7 | 4712.1 | 5429.0 |
Stress area: 271.5 mm² · Proof load: 157,470 N · Clamp load (75%): 118,102 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 472.4 | 348.4 | 4181.1 | 4817.2 |
| Oiled | 0.15 | 354.3 | 261.3 | 3135.8 | 3612.9 |
| Zinc Plated | 0.18 | 425.2 | 313.6 | 3763.3 | 4335.8 |
| Waxed | 0.1 | 236.2 | 174.2 | 2090.5 | 2408.6 |
| MoS₂ | 0.12 | 283.4 | 209.0 | 2508.3 | 2889.9 |
| Galvanized | 0.25 | 590.5 | 435.5 | 5226.4 | 6021.4 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 244.79 mm² = 106,484 N
Step 2 — Torque (dry): T = 0.20 × 0.0200 m × 106,484 N = 425.9 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