Stress area: 156.67 mm² · Proof load: 90,869 N · Clamp load (75%): 68,151 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 218.1 | 160.9 | 1930.3 | 2224.0 |
| Oiled | 0.15 | 163.6 | 120.7 | 1448.0 | 1668.3 |
| Zinc Plated | 0.18 | 196.3 | 144.8 | 1737.4 | 2001.7 |
| Waxed | 0.1 | 109.0 | 80.4 | 964.7 | 1111.5 |
| MoS₂ | 0.12 | 130.9 | 96.5 | 1158.6 | 1334.8 |
| Galvanized | 0.25 | 272.6 | 201.1 | 2412.7 | 2779.8 |
Stress area: 167.25 mm² · Proof load: 97,005 N · Clamp load (75%): 72,754 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 232.8 | 171.7 | 2060.5 | 2373.9 |
| Oiled | 0.15 | 174.6 | 128.8 | 1545.3 | 1780.4 |
| Zinc Plated | 0.18 | 209.5 | 154.5 | 1854.2 | 2136.3 |
| Waxed | 0.1 | 116.4 | 85.9 | 1030.2 | 1187.0 |
| MoS₂ | 0.12 | 139.7 | 103.0 | 1236.4 | 1424.5 |
| Galvanized | 0.25 | 291.0 | 214.6 | 2575.6 | 2967.4 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 156.67 mm² = 68,151 N
Step 2 — Torque (dry): T = 0.20 × 0.0160 m × 68,151 N = 218.1 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