D5.D.6.7 Clause 6.3.1.4 - Slenderness for torsional and torsional-flexural buckling

Equations 6.52 and 6.53 of NF EN 1993-1-1:2005 are to be used to calculate the non-dimensional slenderness λ_T, to be used for torsional and torsional-flexural buckling checks. NF EN 1993-1-1:2005 does not provide equations to calculate the elastic critical loads N_cr,T,F and N_cr,T (refer 6.3.14 of NF EN 1993-1-1:2005).

The NCCI document SN001a-EN-EU: Critical axial load for torsional and flexural torsional buckling modes provides methods to calculate the N_cr,TF and N_cr,T factors and therefore these methods are used to evaluate the elastic critical loads for the French NA.

ねじれ座屈に対する限界軸荷重は以下のように算出されます。

where

$i_{o}^{2}$	=	$i_{y}^{2} + i_{z}^{2} + y_{o}^{2} + z_{o}^{2}$
i_yおよびi_z	=	それぞれ、Y-Y（弱軸）とZ-Z（強軸）についての断面二次半径

曲げねじれ座屈に対する限界軸荷重は以下のように算出されます。

N_{c r, T F} = \frac{i_{o}^{2}}{2 (i_{y}^{2} + i_{z}^{2})} [N_{c r, y} + N_{c r, T} - \sqrt{{(N_{c r, y} + N_{c r, T})}^{2} - 4 N_{c r, y} N_{c r, T} \frac{i_{y}^{2} + i_{z}^{2}}{i_{o}^{2}}}]

これらの式の詳細については、NCCIドキュメントSN001a-EN-EUを参照してください。