C_Lincreases until __________________________ or the ___________________ angle of attack.

At this point, the airfoil is aerodynamically _________________________.

A stall will only occur when the _______________ angle of attack has been exceeded.

Bernoulli's Principle affects lift produced on the ___________________ surface of the wing by accelerating the air and thus reducing its internal pressure.

The ___________________ _______________ is the point where the air molecules slow or stop on the leading edge of the airfoil.

Higher AOAs result in a ______________________ stagnation point on the leading edge.

The representation of the location of all the lifting vectors in a single point is known as the __________________ of ______________________.

Write out the Lift Equation: ________________________________________

The two things the pilot can change in the lift equation are ______________________________ and __________________.

The region where the air either separates or becomes turbulent airflow is the ___________________ region.

In the __________________ region, the flow of air will also circulate back toward the leading edge of the airfoil and form "eddies."

Friction drag becomes greater in the ___________________ boundary layer.

The _________________ flow moves forward closer to the leading edge as the angle of attack ________________________.

Turbulent Air allows for an increase in _______________________ although it is not as useful as laminar flow for lift production.