Definition of Frame

Select the structural frame type (braced/unbraced) with respect to the global X- and Y-directions. Select the auto-calculation option for the effective buckling length factors for column members.

From the Main Menu select Design > General Design Parameter > Definition of Frame.

From the Menu tab of the Tree Menu select Design > General Design Parameter > Definition of Frame.

The following dialog box is used to enter the data:

Definition of Frame dialog box

Definition of Frame

Define the type of structural frame.

X-Direction of Frame
Select Unbraced | Sway or Braced | Non-sway frame in the global X-direction (Default = Unbraced | Sway).

Y-Direction Frame
Select Unbraced | Sway or Braced | Non-sway frame in the global Y-direction (Default = Unbraced | Sway).

Design Type

When members in a 3-D structure are designed, a Design Type is selected to account for only the forces in the selected plane to design the members as a 2-D frame.

3 - D: Design is carried out while accounting for all the member forces in the 3-D frame.

X - Z Plane: Design is carried out while accounting for only the member forces in the GCS X-Z plane as a 2-D frame.

Y - Z Plane: Design is carried out while accounting for only the member forces in the GCS Y-Z plane as a 2-D frame.

X - Y Plane: Design is carried out while accounting for only the member forces in the GCS X-Y plane as a 2-D frame.

Note
This option may become handy when a structure with continuity in one direction is to be designed as a 2-D frame.

Auto Calculate Effective Length Factors

Select if the effective buckling length factors are to be automatically calculated.

Note

• Auto calculation procedure for effective length factor

  (1)  Calculate the stiffness, S (=EI/L), of the members which are connected to the ‘Member a’ as shown in the figure 1 below. If the joint of the flexural member is fixed or hinged as shown in the figure 2 below, the stiffness, S, is modified as below.

   

   

  Fixed joint: S = (1/1.5)* EI/L

  Hinge: S= (1/2.0)* EI/L

   

   

  Where,

   

               E: Modulus of elasticity

  I: Moment of inertia of section

  L: Span length of flexural member measured from center to center of joints

   

  

   

  (2) Calculate Ψ and Ψ. Ψ  is the ratio of Σ(EI/lc) of compression members and Σ(EI/l) of flexural members in a plane at one end of a compression member. As shown in the figure 3 below, if the end of the compression member is fixed or hinged, Ψ is taken as 1 or 10 respectively. If the compression member is not connected to any flexural member, Ψ is taken as 1000.

   

  

   

  (3)  Calculate the solution, X, in the stability equation below.

   

    Braced / Nonsway frames

   

  

   

  Unbraced / Sway frames

   

  

   

  Where, Ψ: Ratio of Σ(EI/lc) of compression members to Σ(EI/l) of flexural members in a plane at one end of a

  compression member.

   

  (4)  Calculate the effective length factor, K

   

  

   

  [Reference: "Steel structures" (1982), Ballio and Mazzolani]

 : Enter the selection and close the dialog box.

 : Do not enter the selection and close the dialog box.