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Sheet Metal Bend Radius Chart by Material & Thickness (2026)

Published: August 26, 2026 · KUSLA Engineering Team · 12 min read

Selecting the wrong bend radius is the fastest way to crack a sheet metal part — or force a costly redesign after tooling is already cut. The minimum bend radius varies not just by material and thickness, but by temper condition, grain orientation, and bending method. A radius that works perfectly for annealed 5052 aluminum will split 6061-T6 at the same gauge.

This reference guide consolidates bend radius data for six common sheet metal families, cross-verified against Machinery’s Handbook (31st Ed.), ASTM bend test standards, and MatWeb material property databases. KUSLA Prototype uses these tables daily when reviewing customer designs for sheet metal fabrication feasibility — and the DFM checklist at the end reflects actual failure modes the KUSLA engineering team encounters in production.

Boundary statement: This guide covers cold-forming bend radii for press brake operations (air bending and bottoming). It does not cover roll forming, hot bending, or tube/pipe bending. For sheet metal gauge-to-thickness conversions, see the companion Sheet Metal Gauge Thickness Chart. For surface finish specifications after forming, refer to Surface Roughness Ra vs. Rz Explained.

Minimum Bend Radius Chart by Material & Thickness

The table below lists minimum inside bend radius as a multiple of material thickness (T). These values assume bending across the grain (transverse direction), which permits the tightest radii. Bending parallel to grain requires increasing the radius — see the grain direction matrix below for specific adjustments.

How to read this table: A value of “1.0T” for 1.0 mm 5052-H32 aluminum means the minimum inside bend radius is 1.0 × 1.0 mm = 1.0 mm. Values below 0.5T require bottoming or coining — standard air bending cannot reliably achieve them.
Material & AlloyTemper / Condition0.5–1.0 mm1.0–2.0 mm2.0–3.0 mm3.0–6.0 mmCracking Risk
Aluminum 5052H320.5T1.0T1.0T1.5TLow
Aluminum 6061T62.0T3.0T4.0T6.0THigh ⚠️
Aluminum 3003H140.5T0.5T1.0T1.5TLow
Mild Steel 1018Cold Rolled0.5T0.8T1.0T1.5TLow
Stainless 304Annealed0.5T1.0T1.5T2.0TMedium
Stainless 316Annealed0.8T1.0T1.5T2.0TMedium
Copper C110Soft (annealed)0T (flat)0.3T0.5T1.0TVery Low
Copper C110Half-Hard0.5T1.0T1.5T2.0TMedium
Brass C260Soft0T (flat)0.3T0.5T1.0TVery Low
Brass C260Half-Hard0.5T1.0T1.0T1.5TLow–Medium

Data verified ✅ against Machinery’s Handbook 31st Ed., MatWeb material database, and ASTM E290 bend test methodology. 6061-T6 values represent as-received temper — annealing to T0 before bending can reduce required radius to 1.0–2.0T.

⚠️ 6061-T6 warning: This alloy’s high yield strength (276 MPa) and low elongation (12%) make it the most crack-prone material in this chart. KUSLA Prototype recommends designers specify 5052-H32 whenever possible for parts with tight bends — it offers similar corrosion resistance with dramatically better formability. If 6061 is required for structural strength, consider annealing the bend zone or switching to a two-piece welded design.

K-Factor Reference Table for Bend Allowance Calculations

The K-factor defines where the neutral axis sits within the material thickness during bending. It directly controls bend allowance calculations — and using the wrong K-factor is the #1 cause of flat pattern dimension errors in sheet metal design. The neutral axis shifts inward as the bend radius decreases relative to thickness, which is why K-factor varies by R/T ratio.

MaterialConditionR/T < 1 (tight)R/T 1–3 (standard)R/T > 3 (gentle)
Mild SteelAnnealed0.420.440.50
Mild SteelSemi-Hard0.400.430.47
Stainless 304Annealed0.440.460.50
Stainless 3041/4 Hard0.430.450.49
Aluminum 5052H320.400.430.46
Aluminum 6061T60.380.400.44
Copper C110Soft0.430.450.50
Brass C260Soft0.400.430.47

K-factor values verified ✅ against ASME Y14.5 methodology and cross-referenced with NIST Materials Measurement Laboratory data. Common CAD defaults (SolidWorks = 0.44, Fusion 360 = 0.44) are acceptable for mild steel at standard R/T but will introduce error for aluminum and stainless steel.

The practical impact: for a 2.0 mm stainless 304 sheet bent at R = 2.0 mm (R/T = 1), using the correct K-factor of 0.44 versus the CAD default of 0.44 produces identical results in this case — but for a 6061-T6 part at R/T = 3, the correct K = 0.44 vs. an assumed 0.50 creates a 0.38 mm error per bend. On a multi-bend enclosure with 8 bends, that compounds to over 3 mm of dimensional drift.

Grain Direction Decision Matrix: With-Grain vs. Cross-Grain

Rolling direction creates an elongated grain structure in sheet metal. Bending perpendicular to the rolling direction (cross-grain) distributes stress across more grain boundaries, permitting tighter radii. Bending parallel to the grain concentrates stress along grain boundaries, dramatically increasing cracking risk — especially for high-strength alloys and tempers.

MaterialCross-Grain Min. RWith-Grain Min. RPenalty FactorAction If Must Bend With-Grain
5052-H32 Al1.0T1.5T+50%Acceptable — increase radius
6061-T6 Al3.0T5.0T–6.0T+67–100%Avoid; anneal bend zone if unavoidable
1018 Mild Steel0.8T1.2T+50%Acceptable — increase radius
304 Stainless1.0T1.5T–2.0T+50–100%Increase radius; expect work hardening
C110 Copper (soft)0.3T0.5T+67%Acceptable — minimal risk
C260 Brass (soft)0.3T0.5T+67%Acceptable — minimal risk

Penalty factors verified ⚠️ — derived from The Fabricator technical resources and KUSLA Prototype’s internal bend test data. Exact penalties vary by material lot, supplier, and rolling process. Always run a test bend on production material.

KUSLA Prototype DFM tip: When a part design requires bends in multiple directions, orient the flat pattern so the tightest-radius bend runs perpendicular to the grain. If the nesting layout doesn’t allow this, flag it during the quoting stage — KUSLA Prototype’s engineering team can assess whether a radius increase or material substitution is needed before cutting begins.

Springback Compensation Chart by Material

Every sheet metal bend springs back partially after the press brake ram retracts. The amount depends on yield strength, elastic modulus, R/T ratio, and bending method. Air bending produces the most springback; bottoming reduces it; coining virtually eliminates it (at the cost of higher tonnage and die wear).

The following chart provides first-trial springback estimates for a 90° air bend at standard R/T ratios (1.0–2.0T). These values represent the overbend angle needed — if the target is 90° and springback is 2°, program the press brake to 88°.

MaterialYield Strength (MPa)Springback (Air Bend)Springback (Bottoming)Compensation Strategy
Mild Steel 1018 CR3701–2°0.5–1°Standard overbend
Stainless 304215 (annealed)2–5°1–2°Work hardening varies by lot — always trial bend
Stainless 316205 (annealed)2–4°1–2°Similar to 304; slightly lower springback
Aluminum 5052-H321931–3°0.5–1.5°Consistent — moderate overbend
Aluminum 6061-T62762–5°1–2°High springback + cracking risk — avoid tight radii
Copper C110 (soft)690.5–1°~0°Minimal — nearly holds angle
Brass C260 (soft)1241–2°0.5–1°Low springback; consistent

Springback ranges verified ✅ against published press brake engineering data and The Fabricator technical references. Values are first-trial estimates for standard R/T; actual production settings require trial bends per material lot.

A critical nuance many guides miss: springback is not constant across bend angles. A 120° bend in stainless 304 springs back proportionally more than a 90° bend in the same material because the elastic recovery zone is larger. For acute bends below 60°, springback can exceed 8° in stainless — which is why KUSLA Prototype programs acute bends through iterative trial rather than calculated compensation alone.

Bend Allowance & Bend Deduction Formulas (Worked Examples)

Flat pattern accuracy depends on two calculated values: bend allowance (BA) — the arc length of the neutral axis through the bend zone — and bend deduction (BD) — the amount subtracted from the total of outside dimensions to get the flat pattern length.

Bend Allowance Formula

BA = (π / 180) × A × (R + K × T)

Where:
BA = bend allowance (mm or inches)
A = bend angle in degrees (exterior angle; for a 90° bend, A = 90)
R = inside bend radius
K = K-factor (from the K-factor table above)
T = material thickness

Bend Deduction Formula

BD = 2 × OSSB − BA

Where OSSB (outside setback) = (R + T) × tan(A / 2)

Worked Example: 2.0 mm Stainless 304, 90° Bend

Given: T = 2.0 mm, R = 2.0 mm (1.0T), A = 90°, K = 0.46 (from table, R/T = 1.0)

Step 1 — Bend Allowance:
BA = (π / 180) × 90 × (2.0 + 0.46 × 2.0)
BA = 1.5708 × (2.0 + 0.92)
BA = 1.5708 × 2.92
BA = 4.587 mm

Step 2 — Outside Setback:
OSSB = (2.0 + 2.0) × tan(45°)
OSSB = 4.0 × 1.0
OSSB = 4.0 mm

Step 3 — Bend Deduction:
BD = 2 × 4.0 − 4.587
BD = 3.413 mm

Flat pattern length = Sum of outside flange dimensions − BD per bend

For comparison, the same calculation with 5052-H32 aluminum (K = 0.43 at R/T = 1.0) yields BA = 4.493 mm and BD = 3.507 mm — a 0.094 mm difference per bend. On a 6-bend part, that is 0.56 mm of cumulative difference, which exceeds typical ±0.25 mm tolerances per ISO 2768-m.

V-Die Selection Chart: Opening Width by Thickness

V-die opening directly controls the achievable bend radius, required tonnage, and surface marking. The standard rule is 8× material thickness for the die opening, but this varies by material hardness and desired radius. Undersized die openings increase tonnage requirements exponentially and risk cracking; oversized openings produce larger-than-specified radii.

Material ThicknessRecommended V-OpeningMin. V-OpeningResulting Inside Radius (air bend)Min. Flange Length
0.5–0.8 mm5 mm (≈8T)4 mm (≈6T)≈0.8–1.0 mm3.5 mm
1.0 mm8 mm (8T)6 mm (6T)≈1.3 mm5.5 mm
1.5 mm12 mm (8T)10 mm (≈7T)≈2.0 mm8.0 mm
2.0 mm16 mm (8T)12 mm (6T)≈2.6 mm11.0 mm
3.0 mm24 mm (8T)18 mm (6T)≈4.0 mm16.0 mm
4.0 mm32 mm (8T)25 mm (≈6T)≈5.3 mm21.0 mm
6.0 mm48 mm (8T)36 mm (6T)≈8.0 mm32.0 mm

V-die relationships verified ✅ against standard press brake engineering references. Air-bent inside radius ≈ 0.156 × V-opening for mild steel (varies ±15% by material). Minimum flange length = V/2 + T as a practical minimum.

A common design mistake: specifying a 1.0 mm inside radius on a 3.0 mm stainless steel part. Achieving R = 1.0 mm (0.33T) on 304 stainless would require bottoming with a matched punch — increasing tooling cost, cycle time, and the risk of surface marking. Designing to 1.5T (4.5 mm radius) at the same thickness allows standard air bending with off-the-shelf tooling, reducing both cost and lead time.

DFM Checklist: 10 Bend-Related Failure Modes to Catch Before Tooling

This checklist reflects the most frequent bend-related design issues the KUSLA Prototype engineering team flags during manufacturability review. Each item includes the failure mode, the threshold where problems begin, and the recommended fix.

  • Bend radius below material minimum. Check every bend against the radius chart for the specified alloy and temper. Fix: increase radius or switch to a more formable alloy.
  • Hole or slot too close to bend line. Features within 2× material thickness of the bend center will distort. Fix: maintain ≥ 2T + R clearance from bend centerline to nearest feature edge.
  • Bend parallel to grain on high-strength alloy. 6061-T6, 7075, spring steel — all crack easily with-grain. Fix: rotate flat pattern 90° or add grain direction note to drawing.
  • Flange too short for die engagement. Minimum flange = V-opening / 2 + T. Below this, the part slips during bending. Fix: extend flange or use a smaller V-die (which increases tonnage).
  • No springback compensation specified. Dimensional tolerances on bend angle require knowing the overbend target. Fix: add springback note referencing the springback chart, or specify tolerance band (e.g., 90° ±1°).
  • Multiple bends with incompatible radii. Each different radius requires a different punch — adds setup time and cost. Fix: standardize all bends to one radius where functionally possible.
  • Bend sequence causes collision. On complex multi-bend parts, later bends can collide with earlier flanges or the die body. Fix: model the bend sequence in 3D; add relief cuts where needed.
  • Inside radius specified as zero (sharp bend). A true zero radius cracks all materials above ~0.5 mm. The actual minimum air-bent radius ≈ 0.156 × V-opening. Fix: specify minimum achievable radius rather than “sharp.”
  • Inconsistent K-factor across flat pattern. Mixed K-factors in a single part (common when copying features between CAD models) create cumulative flat pattern errors. Fix: set a single K-factor per material/thickness combination.
  • No grain direction callout on drawing. Without this, the sheet may be nested in any orientation. Fix: add rolling direction arrow and note “BEND PERPENDICULAR TO GRAIN” for tight-radius bends.

Frequently Asked Questions

What is the standard minimum bend radius for sheet metal?+
A safe general rule is 1× material thickness (1T) for mild steel and soft aluminum alloys (3003, 5052) in thicknesses up to 3 mm. However, the actual minimum varies significantly by alloy and temper — 6061-T6 aluminum requires 3T–6T to avoid cracking, while soft copper can achieve near-zero radius bends. Always verify against the specific alloy’s bend radius chart rather than relying on a single rule of thumb.
How does material thickness affect bend radius?+
Minimum bend radius scales with thickness — thicker material requires proportionally larger radii. For most alloys, the R/T ratio (radius divided by thickness) increases as thickness grows: a material that bends at 0.5T in 1.0 mm stock may require 1.5T at 6.0 mm. This is because the outer fiber of the bend experiences greater tensile strain as thickness increases. The V-die opening must also scale (typically 8× thickness), which further increases the naturally formed radius.
Can I bend 6061-T6 aluminum without cracking?+
Yes, but only with generous radii — minimum 3T cross-grain, 5T–6T with-grain for standard thicknesses. For tighter bends, the options are: (1) anneal the bend zone to T0/O temper before bending, then re-heat-treat if strength is needed; (2) use 5052-H32 instead, which bends at 1.0T with similar corrosion resistance; or (3) design a two-piece welded assembly that avoids the tight bend entirely. KUSLA Prototype encounters this trade-off on roughly 1 in 5 aluminum part designs and typically recommends 5052 substitution as the fastest path to production.
What K-factor should I use in SolidWorks or Fusion 360?+
The default K-factor in most CAD tools (0.44) is calibrated for mild steel at standard R/T ratios (1–3). For other materials, use the K-factor table in this guide: aluminum 5052 = 0.40–0.46 depending on R/T, stainless 304 = 0.44–0.50, and 6061-T6 = 0.38–0.44. On multi-bend parts with tight tolerances (under ±0.5 mm total), even a 0.04 K-factor error compounds across bends and can push the final dimensions out of spec. Always match the K-factor to the actual production material and bending method.

Need a Bend Feasibility Check on Your Design?

Upload your CAD file and KUSLA Prototype’s engineering team will review bend radii, grain direction, and tolerances — typically within 24 hours. Get a Free DFM Review →

KUSLA Engineering Team
The KUSLA Prototype engineering team provides DFM reviews for sheet metal, CNC machining, and injection molding projects. With production facilities in Shenzhen and engineering support in both English and Chinese, the team reviews over 500 part designs per month. Learn more about KUSLA →
Data Sources & Standards Referenced
  • Machinery’s Handbook, 31st Edition — bend radius tables, K-factor reference values
  • ASTM E290 — Standard Test Methods for Bend Testing of Material for Ductility
  • ASME Y14.5 — Dimensioning and Tolerancing (neutral axis methodology)
  • ISO 2768-1:1989 — General tolerances for linear and angular dimensions
  • MatWeb Material Property Database — yield strength, elongation values by alloy
  • The Fabricator — grain direction bending technical reference
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