Stress area: 976.0 mm² · Proof load: 566,080 N · Clamp load (75%): 424,560 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3311.6 | 2442.5 | 29310.1 | 33769.0 |
| Oiled | 0.15 | 2483.7 | 1831.9 | 21982.6 | 25326.8 |
| Zinc Plated | 0.18 | 2980.4 | 2198.2 | 26378.8 | 30391.7 |
| Waxed | 0.1 | 1655.8 | 1221.3 | 14655.1 | 16884.5 |
| MoS₂ | 0.12 | 1986.9 | 1465.5 | 17585.6 | 20260.8 |
| Galvanized | 0.25 | 4139.5 | 3053.1 | 36637.7 | 42211.3 |
Stress area: 1028.4 mm² · Proof load: 596,472 N · Clamp load (75%): 447,354 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3489.4 | 2573.6 | 30883.8 | 35582.1 |
| Oiled | 0.15 | 2617.0 | 1930.2 | 23162.4 | 26686.1 |
| Zinc Plated | 0.18 | 3140.4 | 2316.2 | 27794.9 | 32023.3 |
| Waxed | 0.1 | 1744.7 | 1286.8 | 15441.9 | 17791.1 |
| MoS₂ | 0.12 | 2093.6 | 1544.2 | 18529.9 | 21348.9 |
| Galvanized | 0.25 | 4361.7 | 3217.0 | 38604.3 | 44477.1 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 976.0 mm² = 424,560 N
Step 2 — Torque (dry): T = 0.20 × 0.0390 m × 424,560 N = 3311.6 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