I have an ellipsoid which represents an elliptical wing. It has a chord ($2\times r_A$), a semi-span ($r_C$), and a maximum thickness ($r_B$). Here, $r$ is the radius, and $A$, $B$, and $C$ are the coordinate system based at the base of the ellipsoid.
A global coordinate system is defined $x$, $y$, and $z$. $C$ is always $z$, but $A$ & $B$ are rotations of $x$ and $y$ by some angle $\alpha$. In other words, the test domain is fixed by $x$, $y$ and $z$, but the wing is at some angle-of-attack $\alpha$ to the flow (coming in the positive $x$ direction).
What is the projection (shadow) of the ellipsoid on the $yz$ plane for any $\alpha$?
I know that for $\alpha=0$, the area will be $\pi \times r_C \times r_B$, and should increase as the angle increases as long as $r_A$ is larger than $r_B$. For $\alpha=\pi/2$, the area should be $\pi \times r_C \times r_A$.
Given that $r_C$ will always appear in the equation, I feel the problem may just be working out the projection of the ellipse that is formed at the base of the wing (with radii $r_A$ and $r_B$) on to the $y$ axis.
If this is correct, then the problem is to find the ? in the schematic below.

