The stress tensor varies through the thickness of the element. For a linear model, the stress at the mid-plane can be thought of as the in-plane stress. The difference between the top and bottom stresses is the bending stress.
For a shell element, it is easier to convert these to forces and moments.
These can be defined either by reference to an axis set(opens new window) (global or user defined axes), using the 2D element property axis, or topologically (local axes).
2D element axes are defined by projecting the 2D element property axis on to the element. If set to Local, set the first edge defining the element x, and the first and last edges defining the element xy plane.
Defining 2D element local axes by reference to an axis set results in more consistent local axes in the mesh. When the 2D element property axis is set to other than local, then the specified axis system is projected on to the element.
Note: Look out for: Local axis definition. Adjacent elements may have completely different axis directions making it difficult to interpret results.
Tip: If you aren’t sure about the orientation of the local axes, tick Element axes in the Labels and display methods dialogue box. The axes are coloured Red / Green / Blue for x / y / z.
Note: Forces and moments are given per unit length in the relevant direction. These are essentially the appropriate stresses multiplied by the element thickness. For a 0.5 × 0.5m square element, therefore, you need to multiply the value by 0.5 to get the total force in the element.
These correspond to a 2D tensor based on the bending stresses, aggregated over the thickness of the element.
As in-plane forces and moments are tensor quantities we can define principal forces and moment, similar to principal stresses and maximum shear force and twisting moment.
These are the principal demands in whichever direction they occur and can be projected onto an axis of interest.
When you bend a 2D element you get moments about the two in-plane axes ( and ) and a twisting moment (). These form the basis of projected moments.
Note: Projected refers to the way the output axis set is projected on to the surface of the element.
Maximum and minimum moments are the principal moments, (i.e., projected moments rotated so that the twisting moment is 0).
These are derived; calculated from the basic (projected) moment results and are independent of the axis set.
The same principles apply to the in-plane forces (, & and & ).
Note: The projected moments and are based on the stress in the x and y direction respectively (Timoshenko convention) and are not about the x and y axes.
Projected moments are given relative to the specified axes.
Example: gives moments in the direction of (not about) the x axis. Whether this is the local axis for each element, or the global axis for the whole model is very important. Always check which you are using by clicking the Axes button in the Contour plot dialogue box. This is accessed via the Contour settings icon to the right of the graphic interface.
The local x axis is defined in the direction of the first edge you draw in the 2D element.
Both are signed; the latter refers to principal compression. Look at both results to understand the principal compression/tension regime in each element.
To account for in-plane twisting, use the and results.
This will indicate the maximum force / unit length (GSA doesn’t define an equivalent stress) at all locations. There are likely to be large inaccuracies, especially adjacent to point supports.
Check the results first without averaging stresses and forces at nodes, to ensure the error is small.
If using envelopes, check the envelope method used, located towards the bottom of the Contours dialogue box.
The fundamental result for 2D element is the stress state. This is represented by a tensor which can be thought of as a matrix, where each term corresponds to a force per unit area:
Where the shear terms may be denoted by instead of
We can use Mohr’s circle to understand what is happening in the element, and to the principal stresses.
The three circles correspond to the three pairs of directions x-y, y-z and z-x.
Taking the x-y directions, the centre of the circle is:
And the radius:
Giving principle stresses:
The same applies to the other two direction pairs leading to , and : maximum, intermediate and minimum principal stresses.
The maximum shear stress is simply the largest value of . Plotting the principal stresses give a good indication of the flow of the stresses in the model, but there are still multiple values to consider.
Taking an element with an isotropic material under uniaxial stress we can measure how close to yielding we are by comparing the stress in the element with the yield stress in the material. To compare the general stress state to yield we normally use the von Mises stress(opens new window).
This is defined as:
And in the uniaxial stress state reduces to:
Note:GSA RC design will check if your walls can be reinforced. See Projected demands to do independent checks by hand.
To check shear stresses use the projected stresses. Normally, GSA sets the element axes with y vertical and x horizontal and z out-of-plane. So, the shear stresses that you are interested in are projected xy. A quick hand calculation to check approximate stresses at, e.g., ground level, should confirm that you are looking at the right thing.