GD Pilot Physics MCQs

Solved MCQs of The Lifting Surface Theory for the job of GD Pilot physics MCQs

On the basis of loading, lifting surface problems are evaluated?
(A). True
(B). False
(C). Partially True
MCQ Answer: a


The achievements of powered flights are antedated by the loading of lifting surfaces.
(A). True
(B). False
(C). Partially True
MCQ Answer: a


Over a three-dimensional wing a mathematical model that predicts lift distribution is Prandtl lifting line theory?
(A). True
(B). False
(C). Partially True
MCQ Answer: a


On the platform downwash distribution is regular.
(A). True
(B). False
(C). Partially True
MCQ Answer: a


Smooth edge shapes are formed by the plan.
(A). True
(B). False
(C). Partially True
MCQ Answer: a


The analytically overall amount of lift is difficult to predict.
(A). True
(B). False
(C). Partially True
MCQ Answer: a


Normal velocity is related to subsonic lifting surface theory.
(A). True
(B). False
(C). Partially True
MCQ Answer: a


Along with the whole wingspan, the vortex loses the strength.
(A). False
(B). True
(C). Partially True
MCQ Answer: b


The lift over each wing segment corresponds.
(A). False
(B). True
(C). Partially True
MCQ Answer: a


The distribution of loading is represented by the sum of a finite number.
(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