Display 2D results

Tekla Structural Designer
2021
Tekla Structural Designer

Display 2D results

  1. Open a view and change the view regime to Results View.

    The Results tab is opened on the ribbon.

  2. Set the analysis type and loading for viewing analysis results.
  3. In the 2D Results group, select Results, then from the droplist beneath select the result required.
    OptionDescription
    Mdx top Wood Armer bending along panel x axis, top surface
    Mdx bottom Wood Armer bending along panel x axis, bottom surface
    Mdy top Wood Armer bending along panel y axis, top surface
    Mdy bottom Wood Armer bending along panel y axis, bottom surface
    Bearing pressure Bearing pressure
    Fx Axial force in panel x axis
    Fy Axial force in panel y axis
    Fxy Complimentary in-plane shear
    Fxz Shear in panel z axis in the panel xz plane
    Fyz Shear in panel z axis in the panel yz plane
    Mx Bending along panel x axis
    My Bending along panel y axis
    Mxy Plate torsional moment
    σx top In-plane axial stress in the x direction, top surface
    σy top In-plane axial stress in the y direction, top surface
    τxy top In-plane shear stress, top surface
    σx bottom In-plane axial stress in the x direction, bottom surface
    σy bottom In-plane axial stress in the y direction, bottom surface
    τxy bottom In-plane shear stress, bottom surface
    σx max tension Maximum tension stress in the x direction for both surfaces

    = max (σxtop, σxbottom, 0) ≥ 0

    σy max tension Maximum tension stress in the y direction for both surfaces

    = max (σytop, σybottom, 0) ≥ 0

    σx max compression Maximum compression stress in the x direction for both surfaces

    = min (σxtop, σxbottom, 0) ≤ 0

    σy max compression Maximum compression stress in the y direction for both surfaces

    = min (σytop, σybottom, 0) ≤ 0

    σx in-plane In-plane center stress in the x direction
    σy in-plane In-plane center stress in the y direction
    σx in-plane tension In-plane center tension stress in the x direction

    = max (σxin-plane, 0) ≥ 0

    σy in-plane tension In-plane center tension stress in the y direction

    = max (σyin-plane, 0) ≥ 0

    σx in-plane compression In-plane center compression stress in the x direction

    = min (σxin-plane, 0) ≤ 0

    σy in-plane compression In-plane center compression stress in the y direction

    = min (σyin-plane, 0) ≤ 0

Note: Tooltips are available for the contour plots, by hovering over nodes. These display all the relevant results at the node for the selected loading.
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