The Kutta Condition Online Exam Quiz
The Kutta Condition GK Quiz. Question and Answers related to The Kutta Condition. MCQ (Multiple Choice Questions with answers about The Kutta Condition
How airfoil increases its speed?
Options
A : Flow over the topside
B : Flow over the leading edge
C : Flow over the bottom side
D : Flow over the trailing edge
How many stagnation points on the oval cylinder with non-zero angle of attack?
Options
A : Two
B : Zero
C : More than zero
D : One
How stagnation point on the topside of the airfoil reaches the trailing edge?
Options
A : Due to viscous forces
B : Due to surface forces
C : Due to pressure forces
D : Due to drag forces
How starting vortex is formed?
Options
A : As the airfoil begins to move vortex are formed
B : As the airflows on the airfoil vortex are formed
C : As the airfoil moves against the relative wind vortex are formed
D : As the airflows on the circular body vortex are formed
How the cylinder will vibrate in the wind tunnel test?
Options
A : Due to high pressure
B : Due to low pressure
C : Due to relative pressure
D : Due to fluctuations in the flow
Is high airspeed around the trailing edge causes strong viscous forces?
Options
A : FALSE
B : TRUE
C : -
D : -
Is kutta condition apply to oval shaped body?
Options
A : TRUE
B : FALSE
C : -
D : -
Is lift is created on the airfoil using kutta condition?
Options
A : TRUE
B : FALSE
C : -
D : -
Is the airfoil with a sharp trailing edge move with a positive angle of attack?
Options
A : TRUE
B : FALSE
C : -
D : -
Vortex flow occurs at ___
Options
A : Leading edge
B : Trailing edge
C : Chord
D : Chamber line
Airfoil Characteristics more Online Exam Quiz
Prandtl's Classical Lifting-Line Theory