As far as your "bent air" equation is concerned, your coefficient C is conceptually the same as the lift coefficient Cl, as it must be determined for each air foil. The equation itself describes the "average" behavior of the airfoil, and you hope C will prove to be a constant over some useful range of angles just as Cl is. In fact, this is beginning to look more and more like the lift equation rehashed. I wouldn't be surprised if your C was related to Cl by a constant multiplier. Deductive reasoning? When it leads right back to where we already are?
In the real world an integral part of the behavior of air foils involves drag. You don't consider it. Not doing so means any results you obtain will overstate the efficiency of the systems.GeoM[ Parent ]