Which of the following ensures flow smoothly leaving the trailing edge given the right value of circulation?

A)
Angle of Attack
B)
Kutta Condition
C)
Momentum Theorem
D)
The Shape of the Airfoil

Correct Answer :   Kutta Condition


Explanation : According to the Kutta Condition, for a given angle of attack, the value of circulation around the airfoil is such that the flow leaves the trailing edge smoothly. The velocity at the trailing edge is dependent on the shape of the airfoil.