Incorrect Flight Theory at Federal Aviation Adm

The Federal Aviation Administration presents in the basic text  Aerodynamics for Naval Aviators among Aviation Handbooks and Manuals, the following explanation of the generation of lift of a wing:

• An important phenomenon associated with the production  of lift by an airfoil is the “circulation” imparted to the airstream.
• The generation of lift by an airfoil is dependent upon the airfoil being able to create circulation in the airstream and develop the lifting, pressure distribution on the surface. In all cases, the generated lift will be the net force caused by the distribution of pressure over the upper and lower surfaces of the airfoil.
• If the airfoil is given a positive angle of attack, changes occur in the streamline pattern 
and pressure distribution similar to changes caused by the addition of circulation to a cylinder. The positive angle of attack causes increased velocity on the upper surface with an increase in upper surface suction while the decreased velocity on the lower surface causes a decrease in lower surface suction.

We see that FAA teaches pilots that an airfoil somehow creates circulation which generates velocity difference and thus pressure difference above and below the wing and thus lift,  as the top level of the science of flight. But this is nonsense! Nothing is explained! The natural mystery of flight presenting itself to the innocent uneducated mind, is here only made deeper by introducing a physically incorrect casual connection between circulation and lift.  

Another piece of evidence that aerodynamics education is today in free fall with zero lift and only drag.