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Physics MCQs pdf download

1. What does Kelvin’s Circulation Theorem state in an inviscid and barotropic flow?

(A) Circulation increases with time


(B) Circulation remains constant


(C) Circulation decreases due to viscosity


(D) Circulation depends on turbulence



2. Which assumption is NOT required for Kelvin’s Circulation Theorem to be valid?

(A) Inviscid fluid


(B) Barotropic condition


(C) Conservative body forces


(D) High viscosity



3. What is the nature of circulation in a closed fluid loop according to Kelvin’s Theorem?

(A) Zero circulation at all times


(B) Linearly increasing circulation


(C) Constant circulation


(D) Variable due to temperature



4. The starting vortex is generated due to which of the following?

(A) Flow around the leading edge


(B) Viscous effects near the trailing edge


(C) Rotational flow at stagnation point


(D) Lift at high angles of attack



5. The starting vortex forms when an airfoil:

(A) Is at rest


(B) Begins to move


(C) Reaches sonic speed


(D) Loses lift



6. The bound vortex is associated with:

(A) The airfoil’s surface


(B) The free-stream flow


(C) The far wake


(D) The stagnation point



7. What does the starting vortex ensure according to the circulation theory of lift?

(A) Downwash is eliminated


(B) Bound vortex forms on the wing


(C) Lift is zero


(D) Wake turbulence disappears



8. The total circulation in the system of a starting vortex and a bound vortex is:

(A) Maximum


(B) Infinite


(C) Zero


(D) Equal to lift



9. The starting vortex travels:

(A) Along the surface of the airfoil


(B) Into the wake downstream


(C) Toward the leading edge


(D) Around the tip vortices



10. Which of the following is a result of the starting vortex in steady flight?

(A) Destruction of lift


(B) Creation of turbulence


(C) Generation of a constant bound vortex


(D) Induction of pitching moment



 

Physics MCQs pdf download

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

 

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