shear area calculation

hi all,

How does STAAD.pro calculate the shear area of a section.ie. AX, AY?

In the modify section data base, there is no section modulus about z-axis. what is the coordinate system used in the modifying section database command?

 

  • STAAD calculates the shear area of its own based on the formula provided in the reference manual (refer, section 5.19) and used in both analysis and design. 

    STAAD would calculate the shear stress using the shear areas calculated on the basis of the following for the AISC code:

    1. In Y axis: Ay = depth of the section* web thickness
    2. In Z axis: Az = 2/3 * combined area of the flanges.

    As far as reporting of shear area is concerned, please note that the area reported by STAAD is the shear area considered for the stiffness calculation. These shear areas are used in forming the shear deformation part of the stiffness matrix. Basically, this stiffness shear area is a form factor times the axial area. The form factor is based on the shape of the cross section and for a rectangular area STAAD uses a factor of 2/3 or 0.667. So for example for the W21X48 section,

    The shear area Az = 2 x ( 0.667 x bf x tf )
    bf = width of the flange = 8.14 in
    tf = thickness of the flange = 0.43 in

    Az = 2 x ( 0.667 x 8.14 x 0.43 ) = 4.67 in2

    This is the area that is reported which is the stiffness shear area whereas the area used for design is the combined area of the flanges 2 x bf x tf which is in accordance with the AISC verification manual.

    The shear area terms AY and AZ are used in forming the shear deformation part of the stiffness matrix. Basically, this stiffness shear area is a form factor times the axial area. There are published form factors in Timoshenko & Gere; Roark; or Cowper (for a rectangular area a form factor of about 0.85 is used). STAAD uses these published form factors for simple cross sections if the user or the tables do not supply the shear area.

    The form factor is based on the shape of the cross section. For cross sections whose shape is not known, the form factor has to be "guessed", which means, it can only be approximate.

    Please go through the attached documents for further reference.



    Answer Verified By: Seth Guthrie 

  • Nihesh.N,

    I know the thread is quite old. However, could you guide me to to the exact chapter where this is specified in the AISC code. I can't seeem to locate it.

    Thanks,

  • Hi,

    I know the thread is quite old, but I have some questions about shear area in Staad.Pro. Please find below screen shot of Beam properties and the code check steel design result from STAAD.Pro.

    As you can see there is major difference in Ay and AY calculation.

    1. What is fundamentally different in calculation for Ay and AY (Az and AZ for that matter as well)?
    2. I can understand that Ay and Az are obtained from (depth*web thickness) and (2/3*combined areas of flange) respectively. How about AY and AZ? how are these derived? which specific formula is used?
    3. If i were to create a custom member (e.g. W14X90) but with added 0.5"THK plate along the either side of beam web (between top and bottom flange - hence essentially boxing up the beam), how would the Ay, Az, AY, AZ be affected and calculated?

    Thanks.

    -Morgan-

  • Hi,

    In AISC 360-05 and 360-10 code, same formula is used to calculate the shear area (AY and AZ). For W14X90 section, Ay is (14.02*0.44 =) 6.1688 sqr. inch and AZ is (2/3*2*14.52*0.71 =)13.7456 sqr. inch. The same value is used for design and reported in the design output.