Stress area: 1306.09 mm² · Proof load: 757,532 N · Clamp load (75%): 568,149 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 5113.3 | 3771.4 | 45256.5 | 52141.3 |
| Oiled | 0.15 | 3835.0 | 2828.6 | 33942.6 | 39106.3 |
| Zinc Plated | 0.18 | 4602.0 | 3394.3 | 40731.2 | 46927.5 |
| Waxed | 0.1 | 2556.7 | 1885.7 | 22628.7 | 26071.2 |
| MoS₂ | 0.12 | 3068.0 | 2262.8 | 27154.1 | 31285.0 |
| Galvanized | 0.25 | 6391.7 | 4714.3 | 56571.3 | 65177.4 |
Stress area: 1397.15 mm² · Proof load: 810,347 N · Clamp load (75%): 607,760 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 5469.8 | 4034.3 | 48411.8 | 55776.6 |
| Oiled | 0.15 | 4102.4 | 3025.8 | 36309.3 | 41833.0 |
| Zinc Plated | 0.18 | 4922.9 | 3630.9 | 43571.4 | 50199.8 |
| Waxed | 0.1 | 2734.9 | 2017.2 | 24205.9 | 27888.3 |
| MoS₂ | 0.12 | 3281.9 | 2420.6 | 29047.3 | 33466.2 |
| Galvanized | 0.25 | 6837.3 | 5042.9 | 60515.2 | 69721.3 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 1306.09 mm² = 568,149 N
Step 2 — Torque (dry): T = 0.20 × 0.0450 m × 568,149 N = 5113.3 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