Area Moment of Inertia Calculation

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Area Moment of Inertia Calculation – CAD (FEM is similar) method Vs Classical Hand Calculations method.

In this post we will dig into a few things, one of the most common values (area moment of inertia ‘I’) used in a number of margin of safety calculations, principal area moment of inertia calculation, the orientation of the principal axes, and an example case with pure unsymmetric bending.

First things first, let us do a simple recap of the basics:

  • Moments of inertia are always positive
  • Minimum moments of inertia axes always pass through the center of mass
  • Moments of inertia are a measure of the mass distribution of a body about a set of axes. Think of a rotating ice skater. If the person stretches the arms out, she slows down and speeds up otherwise. Hence the smaller the inertia the more concentrated or closer the mass is about a particular axis.
  • Area moments of inertia are for a particular section or a 2D surface
  • Products of inertia can be positive, negative or zero
  • Products of inertia are a measure of the symmetry of a body about a set of axes. They are zero about any axis normal to a plane of symmetry
  • For any given point on a section, for example the centroid or any other point, there exists a set of axes oriented in such a way that all products of inertia are zero

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Nowadays, it is convenient to simply use either a CAD program like Solid Works, or an FEM pre-processor such as FEMAP to get all the data you need for a given section cut. But do you really understand what data it gives you? We can get the section properties of a given cross section by simply clicking some buttons.

However, every now and then, it is a good idea to revisit or jog your memory back to the classical method of area moment of inertia calculation, and the section center of gravity calculations. But, first let us look at the Solid Works method of getting these section properties.

Solid Works Method:

The following figure illustrates a sample L-Angle cross section highlighted in cyan color. The properties of the section are what we are interested in. The part origin is at the bottom left corner of the selected section. We can also see a custom coordinate system "Custom CSYS" for reference purposes.

L-Angle Unsymmetric Pure Bending
Figure 1: L-Angle Part View for Area Moment of Inertia Calculation

It is logical to guess that the centroid of this surface will not be on the surface itself but somewhere in the top right of the angle. In the 'Evaluate' tab in Solid Works there is an icon to calculate the section properties as shown below.

Solid Works Section Properties Icon
Figure 2: Solid Works Section Properties Icon for Area Moment of Inertia Calculation

After selecting the surface of the section, click the icon circled above. This will bring up a pop up dialog box that will list the section properties as shown in the figure below.

Section Properties SW
Figure 3: Section Properties in Solid Works

So starting from the top in the figure above, we can see the total surface area is 40 in^2. The centroid is at X=5.2 in and Y=2.2 in, as expected, w.r.t the origin of the selected coordinate system in the pull down menu (--default--). The origin of the --default-- coordinate system for this part is at the bottom left corner of the selected section. The following figure illustrates how Solid Works displays the area moment of inertia calculation results on the section.

Section Properties SW View
Figure 4: Area Moment of Inertia Calculation Section, SW CG

Next one down in Figure 3 above is the moments of inertia matrix reported at the centroid. This includes the planar bending and torsional values along the diagonal of the matrix, and the products of inertia in the selected coordinate system. We can see that the products of inertia that involve the 'z' axis are zero.

The reason for this is that the xy plane of this section is the only plane of symmetry. In other words, on each side of the section along 'z' the shape and size of the material is the same. Hence all products of inertia about 'z' are zero. All the values in the matrix are reported in the selected coordinate system (--default-- or part coordinate system in Figure 3). But you could select any other coordinate system, for example the "Custom CSYS". Next down in Figure 3 above, we can see the polar moment of inertia Lzz about 'z'.

Next we can see how the principal area moments of inertia axes are displayed using a pink coordinate system at the centroid. The angle between the selected CSYS and this principal CSYS is -17.3108 Degrees (clockwise is negative) as shown in the Figure 3 above. This is the coordinate system about which all products of inertia Ixy, Iyz and Ixz are zero. The principal moments of inertia are always reported at the centroid about the principal axes.

There is a different set of inertia matrix for each CSYS passing through a given point. There will be one set of axes about which all products of inertia are zero at any given point on the section. But In general the principal axes are different for each point on a section.

Finally, at the bottom of Figure 3 above, since the selected coordinate system (default) origin does not coincide with the section centroid, another 'moments of inertia matrix' is displayed, which accounts for the parallel axis theorem w.r.t the selected output coordinate system (default).

Area Moment of Inertia Calculation - Custom CSYS1:

Let us move the custom CSYS1 to the CG of the section, we will also align this CSYS1 by rotating it about its 'Z' axis by -17.3108 degrees. This aligns it with the principal moments of inertia axes at the CG location. See figure below:

Area Moment of Inertia Calculation Custom CSYS at CG
Figure 5: Area Moment of Inertia Calculation with Custom CSYS1 at CG Aligned with Principal MI Axes

Using the new CSYS1, we will again use Solid Works to calculate the section's area moments of inertia.

Area Moment of Inertia Calculation Custom CSYS at CG MI
Figure 6: Area Moment of Inertia Calculation Custom CSYS aligned at CG, Moments of Inertia

So clearly, all the products of inertia are now zero about the principal axes. The centroid in the custom CSYS1 is at (0,0,0) which is its own origin.

It is noteworthy that in section checks, the section loads and moments are evaluated and extracted from the finite element model at the CG. They are then used in combined stress margin of safety (MS) calculations using these section properties.

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Classical Hand Calculation of Unsymmetric L Angle Pure Bending:

OK so far we have learnt how to measure a given section's properties in a CAD program such as Solid Works (others will be similar, including FEM programs). Now let us dig into a different method using an example problem. The same angle section discussed above is used in the example below (click the link below for more details). The paper works out the moments of inertia and stresses using Classical Hand Calculations for a case of unsymmetric pure bending.

In the paper the following items are calculated:

1) Centroid of the section

2) Area moments of inertia of the section in the X-Y plane coordinate system at the centroid (which is what you see in the first matrix in figure 3 above)

3) Principal area moments of inertia using Mohr's Circle method (which is what you see in the Figure 3 above)

4) Then the angle that the principal axes make with respect to the default X-Y plane coordinate system (-17.3 Degrees in Figure 3 above)

5) And then how we determine the neutral axis angle w.r.t the peincipal axes by setting the axial stresses due to a pure unit bending moment load at the C.G equal to zero

6) Finally the paper wraps it up by calculating the axial stresses at the fiber extremes from the neutral axis

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Surya Batchu
Surya Batchu

Surya Batchu is the founder of Stress Ebook LLC. A senior stress engineer specializing in aerospace stress analysis and finite element analysis, Surya has close to two decades of real world aerospace industry experience. He shares his expertise with you on this blog and the website via paid courses, so you can benefit from it and get ahead in your own career.