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Buckling length of lattice girder bars

Designing a lattice girder

The design of the bars of a truss (lattice girder) structure does not require any special theoretical knowledge: normally, the truss bars are designed as compressed and/or tensioned bars, neglecting bending moments and shear forces. The dimensioning of compression bars is nowadays carried out using a model-based computer procedure. For details, see the knowledge base material Design of columns against buckling. Here, only the determination of the deflection length of the compressed bars is presented.

The most important parameter for the dimensioning of a compressed bar is the slenderness:

$$\overline{\lambda}=\sqrt\frac{Af_y}{N_{cr}}$$

where

$$N_{cr}=\frac{\pi^2El}{(kL)^2}$$

where the buckling length factor k is recommended by EN1993-1-1 to facilitate manual calculations:

Type of the barDirection of bucklingk
chord- in-plane
- out-of-plane
0.9
0.9
bracing- in-plane
- out-of-plane
0.9
1.0

Software using model-based computational methods (e.g. Consteel software) determines the elastic critical force Ncr directly by finite element numerical methods, taking into account the behaviour of the entire lattice girder, instead of the above conservative formula. The following example is intended to illustrate the relationship between the manual design procedure proposed by the standard and the results of the modern model-based numerical procedure.

  • Let the structural model of the lattice girder under consideration be the Consteel model shown in Figure 1.
  • Let the load shown correspond to the design load combination of the girder.
  • Determine the deflection length of the most stressed compressed chord member using finite element numerical stability analysis.
Fig. 1  Structural model and design load combination of the examined lattice girder
(ConSteel software)
Fig. 1  Structural model and design load combination of the examined lattice girder
(Consteel software)

Relationship between procedures

The steps of the calculation are:

Buckling stability analysis

The stability analysis of the elastic model shows the governing buckling mode of the lattice structure and the corresponding elastic critical load factor αcr (Figure 2).

Fig. 2 Buckling mode and critical load factor given by numerical analysis
Fig. 2 Buckling mode and critical load factor given by numerical analysis

We can see that the upper chord of the perfectly elastic model is deflected laterally under load. The load that causes this elastic buckling is the critical load, whose value is given by the product of the design load and the critical load factor αcr=5.99.

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