Aerodynamics Physics Solved MCQs with Answers

Solved MCQs on Prandtl’s Classical Lifting-Line Theory in aerodynamics Physics.

At vertical velocity, can a shed vortex be modeled?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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To make an aircraft wing station, can an additional term be added?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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Over each wing segment, the lift is correspond?
(A). False
(B). True
(C). Partially True
MCQ Answer: a

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The amount of lift that a wing geometry will generate, is it difficult to predict it?
(A). False
(B). True
(C). Partially True
MCQ Answer: b

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Lift distribution over a three-dimensional wing Is predicted by Prandtl lifting line theory?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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Can a change in lift distribution be said as a lift section?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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On a given section of a wing does the local induced change the angle of attack?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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The theory of lifting line is applied to circulation?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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With the concept of circulation can lift distribution over a wing be modeled?
(A). True
(B). False
(C). Partially True
MCQ Answer: a

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In the air, vortex filament cannot terminate or begin?
(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
34. Vortex Sheet Aerodynamics MCQs