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AF111 QUIZ

AF111 QUIZ. THEORY OF FLIGHT. Random Quiz. The answers to these questions were taken from a multiple choice test or quiz… Therefore, the answers were the best of 4 possible choices… so you may be able to come up with an answer that is more specific than the answer given in this quiz… HK!.

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AF111 QUIZ

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  1. AF111 QUIZ THEORY OF FLIGHT

  2. Random Quiz • The answers to these questions were taken from a multiple choice test or quiz… • Therefore, the answers were the best of 4 possible choices… so you may be able to come up with an answer that is more specific than the answer given in this quiz… • HK!

  3. Wing span / mean aerodynamic chord.

  4. Asymmetric thrust effect

  5. The stalling speed is unchanged.

  6. The angle of dihedral • The angle of sweepback

  7. The angle of incidence at the tip will be less than at the root.

  8. Pressure differential between the upper and lower surfaces of the wing creates lift.

  9. Lift Weight Thrust Drag

  10. Centre of Gravity

  11. Centre of Pressure

  12. If speed increases, lift increases.

  13. A decrease in pressure on the top of the wing combined with an increase in pressure on the bottom produces lift.

  14. The relative airflow.

  15. Thrust equals drag.

  16. Chord.

  17. Spar.

  18. With a high aspect ratio, induced drag is relatively small.

  19. The relationship of the span to the man chord.

  20. To provide longitudinal stability.

  21. To counteract the effect of the slipstream.

  22. As airspeed increases, induced drag decreases.

  23. The result of the wing’s work.

  24. The angle at which the wing is inclined to the longitudinal axis.

  25. The angle between the chord and the relative airflow.

  26. A very thin layer of air next to the skin that tends to adhere to the skin and is relatively still.

  27. The body is shaped so that airflow over it is smooth and flows with minimal resistance, thus minimizing drag.

  28. The axis extending lengthwise from nose to tail.

  29. Yes.

  30. Lift decreases and drag increases.

  31. It moves aft.

  32. It increases.

  33. Double.

  34. No.

  35. a) 48 KIAS • b) 40 KTAS • c) 40 KIAS • d) 56 KIAS * Correct answer D

  36. Load factor.

  37. It creates a rotational force opposite to the direction of propeller rotation.

  38. The best glide speed is obtained at the best lift/drag ratio.

  39. Wind does not affect rate of climb.

  40. No. Add 5 to 10 knots depending on the gustiness.

  41. POH

  42. Fully down.

  43. Cruise.

  44. Stability due to features in the a/c design.

  45. The angle the wing makes with the horizontal.

  46. It will yaw left.

  47. Yaw.

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