Torsional (-Flexural) Buckling

The Torsional (-Flexural) Buckling Check is executed according to EN 1993-1-1 art. 6.3.1.4.

In case of an RHS section (Formcode 2) or CHS section (Formcode 3) the check will not be executed and a note will be shown instead.

In case of an I-section (Formcode 1), when the check is not limiting it will not be printed and a note is shown instead. Not limiting is defined here as a unity check lower than the unity check for Flexural Buckling. In case however Flexural buckling can be ignored (due to low compression force or low slenderness) the comparison is done with the unity check of the compression check.

The buckling curve for torsional (-flexural) buckling is taken as the z-z buckling curve according to the table given in "Flexural Buckling".

The value of the elastic critical load Ncr is taken as the smallest of Ncr,T (Torsional buckling) and Ncr,TF (Torsional-Flexural buckling).

For doubly symmetric sections the elastic critical load Ncr is taken equal to Ncr,T.
A section is considered doubly symmetric if the cross-section property Betay = Betaz = 0mm or if the following sections are used:
- I-section (Formcode 1)
- Full Rectangular Section (Formcode 7)
- Full Circular Section (Formcode 11)
- Cold Formed I-Plus Section (Formcode 127)
- Cold-Formed IS-Plus Section (Formcode 128)
- Cold-Formed 2C-Section (Formcode 130)
- Virtual Joists (Formcode 160)

Calculation of Ncr,T

The elastic critical load Ncr,T for torsional buckling is calculated according to Ref.[17].

With:

E

Modulus of Young

G

Shear modulus

It

Torsion constant

Iw

Warping constant

lT

Buckling length for the torsional buckling mode

y0 and z0

Coordinates of the shear center with respect to the centroid

iy

radius of gyration about the strong axis

iz

radius of gyration about the weak axis

Calculation of Ncr,TF

The elastic critical load Ncr,TF for torsional flexural buckling is calculated according to Ref.[17].

Ncr,TF is taken as the smallest root of the following cubic equation in N:

0

With:

Ncr,y

Critical axial load for flexural buckling about the y-y axis

Ncr,z

Critical axial load for flexural buckling about the z-z axis

Ncr,T

Critical axial load for torsional buckling

Sheeting

In case a sheeting is used, independent on which side, the augmented It will be used also in Torsional Buckling.

For more information on sheetings see "Annex D: Use of sheeting  ".

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