Precisely calculate bend allowance (BA), bend deduction (BD), and neutral axis location for sheet metal bending. Includes K‑factor, material tables, and real‑time 2D visualization.
In sheet metal fabrication, when a flat sheet is bent, the material stretches on the outer surface and compresses on the inner surface. The neutral axis is a theoretical line within the material that experiences no net length change. Bend Allowance (BA) is the length of the neutral axis along the bend arc — the extra material needed to achieve the desired bent shape. Accurate BA calculation ensures flat patterns unfold correctly, eliminating scrap and rework.
Where: θ = bend angle (degrees), R = inside bend radius, T = material thickness, K = K‑factor (position of neutral axis: 0 = inner face, 0.5 = center, typical 0.33–0.45).
Bend deduction is the amount subtracted from the sum of flange lengths to obtain the flat pattern length: BD = 2 × (R + T) × tan(θ/2) - BA. For a simple L‑bracket with legs L1 and L2, flat length = L1 + L2 - BD. Our calculator provides BA, BD, and also Outside Setback (OSSB = (R+T) × tan(θ/2)).
| Material | Condition / Thickness | K-Factor Range | Recommended |
|---|---|---|---|
| Mild Steel (CRS) | 0.8 – 3 mm | 0.33 – 0.37 | 0.33 |
| Aluminum 5052/6061 | 1 – 4 mm | 0.40 – 0.45 | 0.42 |
| Stainless Steel 304 | 0.6 – 2 mm | 0.35 – 0.40 | 0.38 |
| Copper / Brass | Soft | 0.45 – 0.50 | 0.48 |
| High-strength steel | 1.5 – 3 mm | 0.30 – 0.33 | 0.31 |
A manufacturer needed to produce 500 stainless steel enclosures with 90° bends, thickness 1.2 mm, inside radius 1.5 mm. Initial flat patterns ignored K-factor variation, resulting in 3 mm gap after bending. Using our calculator with K=0.38 gave BA = 2.77 mm and BD = 2.15 mm, correcting the flat length from 187 mm to 184.7 mm, achieving perfect fit. This reduced rework by 95% and saved $2,800 in material.
In real press brake operations, springback increases the final angle; designers often overbend. Our calculator provides the theoretical BA assuming perfect elastic-plastic behavior. For high-precision aerospace components, additional correction factors (like die opening width, material yield strength) may be required. The K-factor itself varies with bend ratio (R/T) and tooling. For R/T < 1, K tends towards 0.33; for R/T > 5, K can approach 0.5. Always perform bend tests.