Description Usage Arguments Value
Determine maximum compressive axial force in the chords at mid-length of the strut, N_{ch,E_d} [kN]
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 | max_compressive_axial_force_in_chords(
trial_member_size,
member_type,
steel_grade,
k,
L,
n,
Ad,
Lch,
E,
h0,
Ned,
list_reference_tables,
isTopLevel,
DL,
LL,
AL,
TL,
Lcry
)
|
trial_member_size |
Trial member size |
member_type |
member_type, categorical: 'UC' or 'UB' |
steel_grade |
steel_grade [N/{mm}^2], categorical: 'S355' or 'S275' |
k |
Coefficient of length as function of wall rigidity [dimensionless] |
L |
Length between two restraints [m] |
n |
Number of lacing planes, default [n=2] |
Ad |
Section area of diagonal (lacing), [cm^2] |
Lch |
Length of chord of betwen restrains (lace points) [m] |
E |
Young modulus [GPa or GN/m^2] |
h0 |
Distance between centroids of chords [m] |
Ned |
Axial compression Force [kN] |
list_reference_tables |
List of reference tables |
isTopLevel |
Is member located at top level? [boolean] |
DL |
Dead load / self-weight of member [kN/m] |
LL |
Live load / imposed load [kN/m] |
AL |
Accidental Impact Load [kN/m] |
TL |
Temperature load [kN/m] |
Lcry |
critical length about major axis [m] |
N_{ch,E_d} Maximum compressive axial force in the chords [kN]
S_v
N_{cr,ch}
{M_{E_d}}
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