Dust In the Wind: Stress and Strain Results in Workbench Mechanical vs. Mechanical APDL

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Twice in the last week we’ve taken tech support calls in which the users questioned why their stress or strain results were being reported differently in Workbench Mechanical vs. the results from the same results file in /POST1 with ANSYS Mechanical APDL.  After answering those questions it was pretty obvious that a Focus blog entry was in order.  All we needed was a good, relevant example to demonstrate the issues and the explanation.

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First glimpse of approaching dust storm.   All photos by the author.

In case you missed it, the big story here in the Phoenix area this week was our monster haboob, or dust storm.  If you’re not familiar with the term haboob, Wikipedia explains it here:  http://en.wikipedia.org/wiki/Haboob.  In order to have a humongous dust storm, you’ve got to have wind. 

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Stopped in a parking lot to take these pictures – the only camera I had was my phone.

 

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About 3 minutes after this picture was taken the dust storm arrived.

Wind tends to cause damage, but although our recent dust storm is estimated to have been 100 miles wide and up to 10,000 ft. high, we fortunately did not sustain much significant wind damage.  Things that do tend to get mangled, however, are deployed patio umbrellas and portable expanding sunshades.  These sunshades typically retract into a compact size and fit in a zip up carrying case.  Many of us have collections of damaged sun shades that still work via creative application of duct tape, wire, etc.  These inexpensive shades work great for keeping the sun off of us during birthday parties or other outdoor gatherings, but high winds tend to cause the metal members to bend and break, causing the shades to need some field engineering repair if not just a one way trip to the dumpster.

Here is a solid geometry representation of a typical portion of the frame of a representative shade.  It consists of two rectangular hollow members, pinned to each other at the center, with pins at each end that in the full structure would be attached to additional components.

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For simplicity, we fixed the pins on the right side to ground, while those on the left side have an upward bearing load applied to the upper pin and a downward bearing load applied to the lower pin.  These loads tend to cause the members to bend at the central pin.  The bearing loads in our example represent the effect of a strong gust of wind hitting the fabric canopy above the frame, with the load eventually reacting through the frame to stakes that attach the frame to the ground at the bottom.   The main thing to note here is that the applied load is large enough to cause significant plastic deformation, not unlike what one might experience in the real world when one of these structures is subjected to a very strong wind.

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Workbench Mechanical, Coarse Mesh, Peak von Mises Stress is 79,219 psi

 

 

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Same Results File in Mechanical APDL /POST1, Peak von Mises Stress is 83,873 psi

The issue here is that for our initial run with a very coarse mesh, when we view the von Mises stress results in the Mechanical editor and then compare them with the von Mises stress results obtained from the same results file in /POST1 in Mechanical APDL, we notice there is a difference (79.2 ksi vs. 83.9 ksi).  Why is that?  It has to do with how stresses are calculated.  First let’s consider Mechanical APDL and /POST1.  The original graphics display system is known as Full graphics.  Fifteen or twenty years ago ANSYS, Inc. developed a newer graphics display system for MAPDL known as Powergraphics.  There are several differences between these two display systems which affect results quantities. 

ANSYS Mechanical APDL uses PowerGraphics by default, which among other things

only looks at results on the exterior surfaces of the model.  Full Graphics, on the other hand, includesinterior elements in addition to the exterior surfaces when displaying results plots.  Another difference is that with Powergraphics we can vary the number of element facets displayed per element edge with the /efacet command.  The default is one facet per edge but for midside-noded elements we can increase that to two or four.  With Full Graphics we are stuck with one facet per element edge.  Workbench Mechanical uses an algorithm whose results tend to compare more favorably with full graphics, although it apparently displays with 2 facets per element edge.   Another option in MAPDL is to plot nodal (averaged) vs. element (unaveraged) stresses. So, which of all these methods is the correct one?  I would consider them all to be correct, just different.  However, we can use the difference inresults as guideline for our mesh density (as well as the presence of singularities). If there is a significantdifference between PowerGraphics and Full Graphics results in MAPDL, this usually indicates the mesh is too coarse, at least in our region of interest. As the mesh is refined, the difference between the two calculations should decrease.  In WorkbenchMechanical 13.0, we can plot averaged and unaveraged stress and strain result plots.  The choice is made in the details view for a given plot.  A significant differencebetween these two quantities also indicates that mesh refinement is needed. In our shade frame model, we can see that as the mesh is refined, the difference in von Mises stress results decreases, as shown in the table below.

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A similar effect is seen with the von Mises plastic strain results:

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Regarding the mesh densities used, the coarse mesh had an element size of at least 0.05 in. on the member hole at the high stress/strain location,  while the fine mesh had an element size of 0.025 on the same hole.  Another way to look at the mesh refinement is that the coarse model had 20 elements on the hole of interest while the fine mesh had 104 elements on the same hole.  Clearly the coarse mesh in this example was way too coarse for engineering purposes, but this was selected for this article to ensure the effect of different results calculation methods was significant and observable.

So, the bottom line here is that if you see unacceptable differences in stress or strain results using different results calculation methods, it likely means that your mesh, at least in the area of interest, is too coarse.  Try adding mesh refinement and check the results again.  In Mechanical, you can try adding a Convergence item to a scoped result plot to at least partially automate this process.  Just be careful that you don’t include any singularities in your desired convergence region.

If you were expecting a reference to the Kansas song, “Dust in the Wind,” well, I guess this is it.  Fortunately we don’t seem to have many lingering affects of the big dust storm.  The parking lot here at PADT has a thin layer of dirt that’s gradually disappearing.  Once we get a good rain it will all get washed away.

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