EC3/8 Design Library
The BucklingCheckResults type exposes the following members.
Fields
Name  Description  

C1 
Coefficients for current moment diagram
 
C2  
C3  
DMy 
Resulting additional moment about yy axis because of the centroid shift of the effective area relative to the center of gravity of the gross cross section according to 6.2.2.5(4)
 
DMz 
Resulting additional moment about zz axis because of the centroid shift of the effective area relative to the center of gravity of the gross cross section according to 6.2.2.5(4)
 
EulerCriticalLoady 
Critical axial load for flexural (Euler) buckling about yy axis
 
EulerCriticalLoadz 
Critical axial load for flexural (Euler) buckling about zz axis
 
kyy 
Interaction factors according to Table A1, Annex A  Method 1 (EC3, Part 11)
 
kyz  
kzy  
kzz  
M2  
M3 
Internal forces that are used during the buckling resistance calculation
 
Ncompression  
NcrT 
Critical axial load for torsional buckling
 
NcrTF 
Critical axial load for torsional flexural buckling
 
Ratio1 
Capacity ratio of equation 6.61 for member subjected to compression and biaxial bending
 
Ratio2 
Capacity ratio of equation 6.62 for member subjected to compression and biaxial bending
 
RatioLateralTorsionalBucklingForCraneGirder 
Interaction ratio of members subjected to combined bending and torsion
 
SectionClassY 
Section class at the maximum moment point
 
SectionClassZ  
T_FT_Ratio 
Capacity ratio against torsional and torsional flexural buckling under compression force Ncompression.
 
x_T_FT 
Reduction factor for Torsional and flexural torsional buckling, only for open sections
 
xLT 
Reduction factor for lateral torsional buckling under moment about yy axis
 
xy 
Reduction factor x for flexural (Euler) buckling about yy axis
 
xz 
Reduction factor x for flexural (Euler) buckling about zz axis
