Thanks for your effort and I am interested in your math.
I am trying to find an easy way to explain it and I can't. You really need an engineering background to understand where stuff comes from and how to calculate the cross section properties, then the changes are easy to calculate. What you are comparing is the moment of inertia (also called the second moment of area) of the original rectangular cross section and the MOI of the trapped cross section.
I use a section properties calculator built into Autocad to calculate the MOI of each section. It will calculate the section properties of any closed shape, so it is very versatile and fast to use. You can calculate the MOI of complicated shapes by hand but it is very tedious and slow. On top of that, the FG is much stiffer than the core wood so you also need to account for that in the section calculations. I tried to find a free online section properties calculator that will do the same thing but had no luck. There are lots of calculators online, but they only do simple shapes like rectangles, circles, triangles, etc.
Below is how things are calculated once you have the section properties for the untrapped and trapped limb sections.
For the above limb dimensions:
I
original = 0.01898in
4I
trapped = 0.01668in
4For the original rectangular cross section the neutral axis (the axis which the section bends about) is mid thickness because the section is symmetrical.
For the trapped section the neutral axis shifts towards the belly. My calculator gives me the location of the neutral axis. In this case it is 0.01493" off of the mid thickness point. The percentage shift in the neutral axis gives the percentage change in the belly and back stresses. Because the NA shifts towards the belly in this case the belly stresses go down and the back stresses go up.
% change in stiffness = % change in MOI = [0.01668/0.01898] x 100 = 87.9% of the original stiffness
% shift in NA = [0.01493/0.225] x 100 = 6.64% (the 0.225" is half the limb thickness, where the original NA is located)
I'm sure that is clear as mud without the calculations for the section properties, but those are not something I am going to show here. The concepts required to understand how to calculate sections and how to solve for composite beams (those with multiple different materials in them) really do require a number of engineering classes to have a good grasp of.
Mark