Timber Column
Run the calcBackground
The EU timber columns calculator can be used to calculate both the demands as well as the resistance of a straight column.The analysis capabilities include:
- Point Axial and Lateral forces
- Point Moments in the major and minor axis (excluding torsion)
- Line Loads (including linearly varying)
- Distributed Loads (including varying tributary width). For details on tributary widths, refer article 170-what-is-tributary-width
- ULS: Section Bending Moment Capacity (EN 1995-1-1:2004 Cl 6.1.6)
- ULS: Shear Resistance (EN 1995-1-1:2004 Cl 6.1.7)
- ULS: Section Compression And Bending (EN 1995-1-1:2004 Cl 6.2.3 & 6.2.4)
- ULS: Compression / Combined with Bending: Flexural Buckling (EN1995-1-1:2004 Cl 6.3.2)
- ULS: Bending or combined bending & compression: Lateral Torsional stability (EN 1995-1-1:2004 Cl 6.3.3)
- SLS: Deflection analysis
- Softwood and Hardwood Timber
- Laminated Veneer Lumber (LVL)
- Glue Laminated Lumber
Tutorial
In this worked design example, we will go through the design process of a single-story stud wall. It is pinned at the top and bottom (restrained in translation, but not in rotation about the z-z or y-y axis). It is for a residential building and is exposed to Service Class 2. A central batten provides restraint for bending about the Z-axis, but not in the Y-axis (refer snapshot below).
Method & scope
See the exact clause
Calculation method
Structural model and load combinations
The calculator models the timber column as a member under combined axial compression and biaxial bending. Loads are entered by type, permanent (G), variable (Q), wind (W), and EN 1990:2002 governing ULS combinations are generated automatically. Bending moments can be entered directly or received via load linking from beam calculations above. Deformation checks use serviceability combinations.Material partial factor and k_mod
Characteristic strengths are divided by the material partial factor gamma_M and modified by k_mod based on service class (1, 2, or 3) and load duration class. The combination that produces the worst utilization governs. design strength = f_k × k_mod / gamma_MCross-section compression (EN 1995-1-1:2004 Cl 6.1.4)
Design compressive stress sigma_c,0,d = N_d / A is checked against the design compressive strength f_c,0,d. compression utilization = sigma_c,0,d / f_c,0,d ≤ 1.0Bending strength about each axis (EN 1995-1-1:2004 Cl 6.1.6)
Bending stresses about the Y-axis and Z-axis are each checked against their respective design bending strengths. For rectangular sections, the same characteristic bending strength applies to both axes, adjusted by k_mod and gamma_M.Shear strength about each axis (EN 1995-1-1:2004 Cl 6.1.7)
Shear stresses induced by forces in each plane are checked against the design shear strength f_v,d. The effective shear area accounts for the cross-section geometry.Cross-section bending and compression interaction (EN 1995-1-1:2004 Eq 6.19 and 6.20)
When axial compression and biaxial bending are combined, the cross-section interaction is checked through two simultaneous equations (Eq 6.19 and 6.20) that weight the demands by the km factor: interaction = sigma_c,0,d/f_c,0,d + sigma_m,y,d/f_m,y,d + km × sigma_m,z,d/f_m,z,d ≤ 1.0 interaction = sigma_c,0,d/f_c,0,d + km × sigma_m,y,d/f_m,y,d + sigma_m,z,d/f_m,z,d ≤ 1.0Flexural buckling interaction (EN 1995-1-1:2004 Cl 6.3.2, Eq 6.23 and 6.24)
Compressive resistance is reduced by the buckling factor k_c,y (about Y-axis) and k_c,z (about Z-axis), each derived from the relative slenderness lambda_rel,c for that axis. The combined flexural-buckling and bending interaction is checked as: interaction = sigma_c,0,d / (k_c,y × f_c,0,d) + sigma_m,y,d/f_m,y,d + km × sigma_m,z,d/f_m,z,d ≤ 1.0 interaction = sigma_c,0,d / (k_c,z × f_c,0,d) + km × sigma_m,y,d/f_m,y,d + sigma_m,z,d/f_m,z,d ≤ 1.0Lateral torsional buckling interaction (EN 1995-1-1:2004 Cl 6.3.3, Eq 6.35)
When the compression face of the column is unrestrained against lateral movement, lateral torsional buckling is checked. The stability factor k_crit is applied to the major-axis bending strength, and the interaction with axial compression is checked per Eq 6.35: interaction = (sigma_m,y,d / (k_crit × f_m,y,d))² + sigma_c,0,d / (k_c,z × f_c,0,d) ≤ 1.0Deformation checks (EN 1995-1-1:2004 Cl 2.2.3)
Governing instantaneous and final (creep-adjusted) deformations are computed for bending about each axis independently. All four combinations (instantaneous Y, instantaneous Z, final Y, final Z) are checked against span-ratio limits from EN 1995-1-1:2004 Table 7.2 and any user-defined absolute limits.Load linking
The column’s base reaction is exported as a linked output to connected footing calculations. Axial load at the column top can be linked from beam reactions above, completing the full load path from beam to column to footing automatically.How to use it
Create a Calculation

Entering our key properties
First, we enter the key properties of our column:- Member Type - Clicking “Select” will open a list of all properties and allow you to select timber sizes from a database, or custom dimensioned timber. Refer to related article Quickly finding the best section with the member selector. We want to use custom dimensions Softwood Timber of grade C20, and select a dimension based on past experience:

- Total Column Length - Select the length between the start and end of the column. We select 3500 mm.
- Critical Buckling Lengths - We are confident that the column has adequate lateral bracing at the batten (braced about z-z axis as per diagram above), so the length between lateral restraints is equal to half the column length (1750 mm).
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- Position of Supports from Bottom - The support conditions may be at any position along the column, and can include 1 or more supports. A cantilever can be created on either end by moving the support condition away from “0” or the “Total Span Length”. In our case, the default simply supported position is adequate.

Load Details
- Distributed Loads (kPa)
- Line Loads (kN/m)
- Point & Moment Loads (kN or kNm)
- Enter the start and end location. Note you can type the ID of any variable, or even include a formula in each input cell. In our case “L” is sufficient.
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Enter the start and end load width. Refer 170-what-is-tributary-width for further details.





Deflection limits: These depend on the national annex and the use of the structure. In the UK annex Table NA.5 BS EN1995-1-1:2004+A1:2008 only beam deflection limits are given. In our case, we know that the wind load will not cause significant lateral bending and we can ignore the calculation. We may set arbitrarily high deflection limits to ensure the check will not exceed any deflection requirements:

- Section selection
Summary of results and internal force diagrams


We can also see the “factored” loads applied for each load combination. We can see that the G = 0.5 kN and QI = 2 kN loads were factored by 1.35 x and 1.5x respectively giving us 3.68 kN total factored axial load. Also, the distributed loads and self-weight were converted to a line load and factored.

Printing and Member Schedule




A more in-depth look
Detailed Mode

Multiple Laminations

Axial Load Eccentricity
Do you sometimes need to check for the axial load being positioned eccentrically to your column, and thereby inducing some bending moment? This is easy to do by selecting from various predefined options in “Default Axial Load Eccentricity”, or even assigning eccentricities per load case.
Available presets
Each preset opens the calculator with a typical setup already entered.Common questions
What design standard does this calculator use?
What design standard does this calculator use?
How do I define a timber section?
How do I define a timber section?
What checks and outputs does it produce?
What checks and outputs does it produce?
How are the combined interaction checks structured?
How are the combined interaction checks structured?
How are flexural buckling lengths handled for each axis?
How are flexural buckling lengths handled for each axis?
Does this calculator support load linking with beam and footing calculations?
Does this calculator support load linking with beam and footing calculations?