Stress area: 1757.73 mm² · Proof load: 1,019,483 N · Clamp load (75%): 764,613 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 7952.0 | 5865.1 | 70381.2 | 81088.1 |
| Oiled | 0.15 | 5964.0 | 4398.8 | 52785.9 | 60816.1 |
| Zinc Plated | 0.18 | 7156.8 | 5278.6 | 63343.0 | 72979.3 |
| Waxed | 0.1 | 3976.0 | 2932.5 | 35190.6 | 40544.1 |
| MoS₂ | 0.12 | 4771.2 | 3519.1 | 42228.7 | 48652.9 |
| Galvanized | 0.25 | 9940.0 | 7331.4 | 87976.5 | 101360.2 |
Stress area: 1828.6 mm² · Proof load: 1,060,588 N · Clamp load (75%): 795,441 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 8272.6 | 6101.6 | 73218.7 | 84357.4 |
| Oiled | 0.15 | 6204.4 | 4576.1 | 54913.6 | 63267.5 |
| Zinc Plated | 0.18 | 7445.3 | 5491.4 | 65896.5 | 75921.2 |
| Waxed | 0.1 | 4136.3 | 3050.8 | 36609.4 | 42178.7 |
| MoS₂ | 0.12 | 4963.6 | 3661.0 | 43931.6 | 50614.8 |
| Galvanized | 0.25 | 10340.7 | 7626.9 | 91523.0 | 105446.2 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 1757.73 mm² = 764,613 N
Step 2 — Torque (dry): T = 0.20 × 0.0520 m × 764,613 N = 7952.0 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