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
MCQ Answer: a

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

MCQ Answer: a

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
MCQ Answer: a

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

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
MCQ Answer: a

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

MCQ Answer: a

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

MCQ Answer: a

On which of the following Vortex flow occurs?
(A). Leading-edge
(B). Trailing edge
(C). Chord
(D). Chamber line
(E). None of these
MCQ Answer: b

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

MCQ Answer: a

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

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

MCQ Answer: a

On the oval shaped body, the Kutta condition is applied?
(A). True
(B). False
(C). Partially True

MCQ Answer: a

Aerodynamics MCQs

1. Infinitesimal Fluid Element
2. Kelvin’s Circulation Theorem and the Starting Vortex
3. Laminar Flow MCQs
4. Lifting Flow over Cylinder MCQs
5. FRCR Physics MCQs
6. Non-lifting Flow over Arbitrary Bodies MCQs
7. Pathlines, Streamlines, Streaklines Physics MCQs
8. Pitot Tube MCQs Physics
9. Classical Lifting-Line Theory MCQs
10. Doublet Flow MCQs
11. Flow in Duct 
12. Continuity Equation MCQs
13. Cambered Airfoil MCQs
14. Kutta Condition MCQs
15. Lifting Surface Theory MCQs
16. Symmetric Airfoil MCQs
17. The Vortex Filament, Biot-Savart Law, Helmholtz Theorem MCQs
18. IAF Physics MCQs
19. Viscous Flow MCQs
20. Uniform and Turbulent Flow MCQs
21. Three Dimensional Source and Three Dimensional Doublet MCQs
22. Vortex Sheet MCQs 
23. Pressure Coefficient MCQs 
24. Source Flow MCQs 
25. Angular Velocity, Strain and Vorticity MCQs
26. Bernoulli’s Equation MCQs
27. MCQs on Circulation
28. Finite Control Volume Approach MCQs
29. Flow over Sphere MCQs
30. Airfoil Characteristics MCQs
31. Downwash and Induced Drag MCQs
32. Aerodynamics MCQs
33. Airfoil Nomenclature MCQs