Stress area: 560.59 mm² · Proof load: 325,142 N · Clamp load (75%): 243,857 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1463.1 | 1079.1 | 12949.5 | 14919.5 |
| Oiled | 0.15 | 1097.4 | 809.4 | 9712.8 | 11190.4 |
| Zinc Plated | 0.18 | 1316.8 | 971.2 | 11654.7 | 13427.7 |
| Waxed | 0.1 | 731.6 | 539.6 | 6475.2 | 7460.3 |
| MoS₂ | 0.12 | 877.9 | 647.5 | 7770.1 | 8952.1 |
| Galvanized | 0.25 | 1828.9 | 1348.9 | 16187.1 | 18649.7 |
Stress area: 621.2 mm² · Proof load: 360,296 N · Clamp load (75%): 270,222 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1621.3 | 1195.8 | 14349.7 | 16532.7 |
| Oiled | 0.15 | 1216.0 | 896.9 | 10762.5 | 12399.8 |
| Zinc Plated | 0.18 | 1459.2 | 1076.3 | 12915.0 | 14879.8 |
| Waxed | 0.1 | 810.7 | 597.9 | 7175.3 | 8266.9 |
| MoS₂ | 0.12 | 972.8 | 717.5 | 8610.0 | 9919.8 |
| Galvanized | 0.25 | 2026.7 | 1494.8 | 17937.8 | 20666.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 560.59 mm² = 243,857 N
Step 2 — Torque (dry): T = 0.20 × 0.0300 m × 243,857 N = 1463.1 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