PHYSICS MCQS for ATC

By: Prof. Dr. Fazal Rehman | Last updated: May 20, 2025

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1. : Over an arbitrary body, the purpose of non-lifting flow is to find ________



2. : Over a given panel why is source strength ‘X’ per unit length constant?



3. : At the rth control point, which of the following is a normal component of the flow velocity?



4. : When sin θ = 0, which of the following will be the shape of Rankine oval?



5. : The function of stream can be obtained by ____



6. : Which of the following is flow past a cylinder?



7. : When U*y + (−u/2πr) = 0, which of the following will be the shape of Rankine oval?



8. : Doublet flow and uniform flow combination gives flow _____



9. : By substituting ____ the shape of Rankine oval of equal axes can be found out?



10. : In the flow over a cylinder, the amount of lift will be generated _________



 

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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