# Online Physics MCQs

Solved Online MCQs of Kutta Condition in Aerodynamic Physics.

With the non-zero angle of attack how many stagnation points are on the oval cylinder?
(A). Two
(B). Zero
(C). More than zero
(D). One
(E). None of these

Strong viscous force is caused by high airspeed around the trailing edge?
(A). False
(B). True
(C). Partially True

The starting vortex is formed as the?
(A). Airfoil begins to move vortex is shaped
(B). Airflow on the airfoil vortex is shaped
(C). Airfoil moves against the relative wind vortex is shaped
(D). Airflow On the circular body vortex is shaped
(E). None of these

The speed of airfoil is increased by Flow over?
(A). The topside
(C). The bottom side
(D). The trailing edge
(E). None of these

On the top side of the airfoil how the stagnation point is reached to the trailing edge?
(A). Due to viscous forces
(B). Due to surface forces
(C). Due to pressureforces
(D). Due to drag forces
(E). None of these

With sharp corners, Kutta condition is applied to solid bodies.
(A). True
(B). False
(C). Partially True

With a sharp trailing edge, the airfoil moves with a positive angle of attack.
(A). True
(B). False
(C). Partially True

On which of the following Vortex flow occurs?
(B). Trailing edge
(C). Chord
(D). Chamber line
(E). None of these

By using Kutta condition the lift is created on the airfoil?
(A). True
(B). False
(C). Partially True

Circulation will be created by the body with a sharp trailing edge.
(A). False
(B). True
(C). Partially True

Flow pattern on the body is referred to by Kutta condition.
(A). True
(B). False
(C). Partially True