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D10.B.11 Design Parameters

Design per Mexican Standards is requested by using the CODE. Other applicable parameters are summarized in Table 13B.1 below. These parameters communicate design decisions from the engineer to the program and thus allow the engineer to control the design process to suit an application's specific needs.

The default parameter values have been selected such that they are frequently used numbers for conventional design. Depending on the particular design requirements, some or all of these parameter values may be changed to exactly model the physical structure.

The parameters DMAX and DMIN may only be used for member selection only.

Note: Once a parameter is specified, its value stays at that specified number until it is specified again. This is the way STAAD.Pro works for all codes.
Table 1. Design Parameters According to Mexican NTC Standards - Steel
Parameter Name Default Value Description
CODE -

Must be specified as MEXICAN.

Design code to follow. See TR.48.1 Parameter Specifications.

BEAM 0

0: Design at ends and those locations specified by  SECTION  command.

1: Design at ends  and at every  y cada 1/12th point along member length

CB 1 Coefficient C defined per section 3.3.2.2. If Cb is set to  0.0 it will be calculated by the program according to  LRFD USA (CbMex=1/CbUSA). Any other value will be directly used in the design.
CMB 1

Cfactor for combined forces when there are transverse loads in the members. Section 3.4.3.3.ii of NTC

  • CMB 1.0 = Members ends are restricted angularly.
  • CMB 0.85 = Members ends are not restricted angularly.
DFF None(Mandatory for deflection check, TRACK 4.0)

"Deflection Length" / Maxm. allowable local deflection

See Note 1 below.

DJ1 Start Jointof member

Joint No. denoting starting point for calculation of "Deflection Length ."

See Note 1 below.

DJ2 End Joint of member

Joint No. denoting end point for calculation of "Deflection Length."

See Note 1 below.

DMAX 114 cm Maximum allowable depth
DMIN 0.0 cm Minimum allowable depth
DSD T

Perform the ductile seismic design in accordance with Section 11 (True or False).

Main design conditions are  considered (not including, at the moment, geometric  ones)

FU 4,230 Kg/cm2 Ultimate tensile strength of steel
FYLD 2,530 kg/cm2 Minimum Yield strength of steel
IMM 0

Main or secondary member for the purpose of checking slenderness

  • 0. Main member 
  • 1. Secondary and wind trusses
INO 0

Curve Definition according to  NTC.3.2.2.1a, defined for I shapes or tubes 

  • 0. n=1.4, laminated I shapes, tubes or built up with 3 or 4 welded plates obtained from wider plates cuts with oxygen.
  • 1. n=1, I shapes, tubes or built up with 3 or 4 welded plates
IRR 0

Variable defined for the whole structure indicating if it is regular or irregular according to section 3.4 of the NTC.

  • Columns that are part of regular structures
  • Columns that are part of irregular structures
KX 1.0 Effective length factor for  flexural-torsional buckling
KY 1.0 Effective length factor for local Y axis- Usually minor axis
KZ 1.0 Effective length factor for local Z axis- Usually major axis
LDR T Defines if the structure has  elements to bear the wind load (shear walls, wind trusses, or bracing rigid elements ) that restrict lateral displacements and allow to disregard slenderness effects. (True or False)
LX Member length Length for determining flexural-torsional buckling
LY Member length Length to calculate slenderness ratio for buckling about  local Y axis.
LZ Member length Length to calculate slenderness ratio for buckling about  local Z axis.
NSF 1 Net section factor for tension members
RATIO 1.0 Permissible ratio of actual load effect and design strength
STIFF Longer of Member length or depth Spacing of stiffeners for beams for shear design
TRACK 0

Controls the level of detail in output

  • 0. = Suppress all design strengths 
  • 1. = Print all design strengths 
  • 2. = Print expanded design output
UNB Member length

Unsupported length (L) of the bottom* flange for calculating flexural strength .  Will be used only if compression is in the bottom flange.

See Note 2 below.

UNT Member length

Unsupported length (L) of the top* flange for calculating flexural strength .  Will be used only if compression is in the top flange.

See Note 2 below.

D10.B.11.1 Notes

  1. For deflection check, parameters DFF, DJ1, and DJ2 from D3.B.6 Design Parameters may be used. All requirements remain the same.
  2. Top and Bottom represent the positive and negative side of the local Y axis (local Z axis if SET Z UP  is used).