Stress area: 1120.9 mm² · Proof load: 650,122 N · Clamp load (75%): 487,592 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 4095.8 | 3020.9 | 36250.9 | 41765.7 |
| Oiled | 0.15 | 3071.8 | 2265.6 | 27187.7 | 31323.8 |
| Zinc Plated | 0.18 | 3686.2 | 2718.8 | 32625.6 | 37588.9 |
| Waxed | 0.1 | 2047.9 | 1510.5 | 18125.5 | 20882.8 |
| MoS₂ | 0.12 | 2457.5 | 1812.6 | 21750.7 | 25059.6 |
| Galvanized | 0.25 | 5119.7 | 3776.1 | 45313.2 | 52206.6 |
Stress area: 1205.7 mm² · Proof load: 699,306 N · Clamp load (75%): 524,480 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 4405.6 | 3249.4 | 38992.9 | 44924.8 |
| Oiled | 0.15 | 3304.2 | 2437.1 | 29244.6 | 33693.6 |
| Zinc Plated | 0.18 | 3965.1 | 2924.5 | 35094.1 | 40432.9 |
| Waxed | 0.1 | 2202.8 | 1624.7 | 19496.4 | 22462.4 |
| MoS₂ | 0.12 | 2643.4 | 1949.7 | 23396.1 | 26955.3 |
| Galvanized | 0.25 | 5507.0 | 4061.8 | 48741.1 | 56156.0 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 1120.9 mm² = 487,592 N
Step 2 — Torque (dry): T = 0.20 × 0.0420 m × 487,592 N = 4095.8 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