Eurocode 9 Aluminium Design Calculator (EN 1999-1-1)

Preliminary member check for aluminium beams and columns according to Eurocode 9 (EC9). Enter geometry, alloy properties and design actions to get utilisation ratios and pass/fail status.

EC9 Member Check

1. Design situation

Default values per EN 1999-1-1; check your National Annex.

2. Aluminium alloy

Values are indicative; always verify with EN 1999-1-1 and product certificates.

3. Section properties

Use gross section properties. For thin-walled sections, local buckling may govern and is not fully covered here.

4. Design actions (ULS)

χ = 1.0 for members without buckling; otherwise obtain from EC9 buckling curves.

Results

Bending resistance

MRd: kNm

Utilisation ηM = MEd / MRd =

Axial resistance

NRd: kN

Utilisation ηN = NEd / NRd =

Shear resistance

VRd: kN

Utilisation ηV = VEd / VRd =

Note: This tool uses simplified expressions based on EN 1999-1-1 for compact sections and does not replace a full code check. See the explanation below for formulas and assumptions.

How the Eurocode 9 aluminium design check works

Eurocode 9 (EN 1999-1-1) provides rules for the design of aluminium structures, including material properties, cross-section classification, member resistance and stability. This calculator focuses on a simplified member check for prismatic members in bending, axial force and shear.

1. Material strengths and partial factors

For a given aluminium alloy and temper, Eurocode 9 defines characteristic strengths:

  • 0.2% proof strength \( f_{0.2,k} \) (analogous to yield strength)
  • Ultimate tensile strength \( f_{u,k} \)

Design strengths are obtained by dividing by material partial factors:

\[ f_{0.2,d} = \frac{f_{0.2,k}}{\gamma_{M1}}, \qquad f_{u,d} = \frac{f_{u,k}}{\gamma_{M2}} \]

Typical default values (subject to National Annex) are:

  • \( \gamma_{M1} = 1.10 \) for member resistance in bending and axial force
  • \( \gamma_{M2} = 1.25 \) for shear and net section checks

2. Bending resistance \( M_{Rd} \)

For a compact cross-section where the full plastic or elastic moment can be developed without local buckling, a simplified design bending resistance about the major axis is:

\[ M_{Rd} = \frac{f_{0.2,k}}{\gamma_{M1}} \, W_y \]

where:

  • \( W_y \) is the section modulus about the relevant axis.

In the calculator, you enter \( W_y \) in cm³; it is internally converted to m³ and combined with \( f_{0.2,k} \) in MPa to give \( M_{Rd} \) in kNm.

The utilisation ratio in bending is:

\[ \eta_M = \frac{M_{Ed}}{M_{Rd}} \]

3. Axial resistance \( N_{Rd} \)

For a member in compression, Eurocode 9 requires a buckling check. This is usually expressed with a reduction factor \( \chi \) obtained from buckling curves:

\[ N_{b,Rd} = \chi \, \frac{f_{0.2,k}}{\gamma_{M1}} \, A \]

The calculator lets you input \( \chi \) directly (default 1.0 for no buckling reduction). The utilisation is:

\[ \eta_N = \frac{N_{Ed}}{N_{Rd}} \]

4. Shear resistance \( V_{Rd} \)

For webs not susceptible to shear buckling, a simplified shear resistance is:

\[ V_{Rd} = \frac{f_{0.2,k}}{\sqrt{3}\,\gamma_{M2}} \, A_w \]

where \( A_w \) is the effective shear area of the web. The utilisation ratio is:

\[ \eta_V = \frac{V_{Ed}}{V_{Rd}} \]

5. Combined bending and axial force

Eurocode 9 includes interaction formulas for combined bending and axial force. For simplicity, this tool reports separate utilisation ratios for bending and axial force. As a conservative quick check, you can ensure:

\[ \eta_M + \eta_N \leq 1.0 \]

For final design, use the exact interaction expressions in EN 1999-1-1, considering cross-section class and buckling mode.

6. Limitations and good practice

  • Only prismatic members with uniform properties are considered.
  • Local buckling, lateral–torsional buckling and joint design are not explicitly checked.
  • Fatigue, serviceability (deflections, vibrations) and fire design are outside the scope of this tool.
  • Always confirm alloy properties and partial factors with the relevant National Annex and product data.

Worked example

Consider a simply supported aluminium beam with:

  • Alloy: EN AW-6060 T6, \( f_{0.2,k} = 190 \) MPa
  • Section modulus: \( W_y = 200 \,\text{cm}^3 \)
  • Shear area: \( A_w = 10 \,\text{cm}^2 \)
  • Area: \( A = 20 \,\text{cm}^2 \)
  • Design actions: \( M_{Ed} = 20 \,\text{kNm} \), \( V_{Ed} = 30 \,\text{kN} \), \( N_{Ed} = 0 \)
  • \( \gamma_{M1} = 1.10 \), \( \gamma_{M2} = 1.25 \), \( \chi = 1.0 \)

Design bending resistance:

\[ W_y = 200 \,\text{cm}^3 = 200 \times 10^{-6} \,\text{m}^3 = 2.0 \times 10^{-4} \,\text{m}^3 \]

\[ M_{Rd} = \frac{190}{1.10} \times 2.0 \times 10^{-4} \approx 34.5 \,\text{kNm} \]

\[ \eta_M = \frac{20}{34.5} \approx 0.58 \]

Design shear resistance:

\[ A_w = 10 \,\text{cm}^2 = 10 \times 10^{-4} \,\text{m}^2 = 1.0 \times 10^{-3} \,\text{m}^2 \]

\[ V_{Rd} = \frac{190}{\sqrt{3}\times 1.25} \times 1.0 \times 10^{-3} \approx 87.8 \,\text{kN} \]

\[ \eta_V = \frac{30}{87.8} \approx 0.34 \]

Both utilisation ratios are below 1.0, so the member passes this simplified EC9 check in bending and shear.

FAQ

Is this calculator suitable for thin-walled extrusions?

Many aluminium structures use thin-walled extruded profiles where local buckling and class 4 behaviour are critical. This tool does not perform effective width calculations or local buckling checks, so it should only be used for preliminary sizing. For thin-walled sections, use manufacturer software or detailed EC9 procedures.

Can I change units?

The calculator works internally in SI units (MPa, m, kN, kNm). Inputs for section properties are in cm² and cm³ for convenience, and are automatically converted. Design actions are entered directly in kN and kNm.

How should I choose the buckling factor χ?

The buckling reduction factor χ depends on the member slenderness, end conditions and buckling curve for the relevant axis and alloy. Eurocode 9 provides buckling curves and formulas to compute χ. For short members or members braced against buckling, χ may be close to 1.0; for slender columns, χ can be much lower.