Stress area: 693.55 mm² · Proof load: 402,259 N · Clamp load (75%): 301,694 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1991.2 | 1468.6 | 17623.6 | 20304.7 |
| Oiled | 0.15 | 1493.4 | 1101.5 | 13217.7 | 15228.5 |
| Zinc Plated | 0.18 | 1792.1 | 1321.8 | 15861.4 | 18274.4 |
| Waxed | 0.1 | 995.6 | 734.3 | 8811.8 | 10152.3 |
| MoS₂ | 0.12 | 1194.7 | 881.2 | 10574.0 | 12182.6 |
| Galvanized | 0.25 | 2489.0 | 1835.8 | 22029.5 | 25380.8 |
Stress area: 760.85 mm² · Proof load: 441,293 N · Clamp load (75%): 330,970 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2184.4 | 1611.1 | 19333.6 | 22274.8 |
| Oiled | 0.15 | 1638.3 | 1208.3 | 14500.2 | 16706.1 |
| Zinc Plated | 0.18 | 1966.0 | 1450.0 | 17400.6 | 20047.7 |
| Waxed | 0.1 | 1092.2 | 805.6 | 9666.8 | 11137.4 |
| MoS₂ | 0.12 | 1310.6 | 966.6 | 11599.8 | 13364.5 |
| Galvanized | 0.25 | 2730.5 | 2013.9 | 24167.0 | 27843.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 580 MPa × 693.55 mm² = 301,694 N
Step 2 — Torque (dry): T = 0.20 × 0.0330 m × 301,694 N = 1991.2 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