Doubled checked the wing area calculation script. Everything seems legit enough.

Next steps:
	Make the swept wing's cross-section parallel to the y&z axis.
	Cut out the ailerons.
	Place placeholders for the servo motors and aileron actuator arms.
Temporary commit. Please amend. Getting ready to implement for loop.
Started moving all my OpenSCAD code over to CoffeeSCAD. CoffeeSCAD seems to be such a better scripted application. It allows for many recursive functions that will prove very helpful.

In addition, I moved some of the outdated CAD files out of the way.