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Aerodynamics & Systems

5 free sample questions of the 53 in this topic. The full set is in the app.

  1. Question 1

    A wing stalls because:

    • A.Airspeed is below a fixed number
    • B.The critical angle of attack is exceeded
    • C.The engine loses power
    • D.The altitude is too high
    Show answer & explanation
    Answer: B. The critical angle of attack is exceeded

    A stall is caused by exceeding the critical AOA. Stalls can occur at any airspeed, attitude, or power setting.

  2. Question 2

    What is the load factor in a coordinated, level turn at a 60° bank?

    • A.1.0
    • B.1.41
    • C.2.0
    • D.3.0
    Show answer & explanation
    Answer: C. 2.0

    Load factor in a level turn is 1/cos(bank). At 60°, cos = 0.5, so load factor = 2.0 Gs.

  3. Question 3

    What happens to stall speed as load factor increases?

    • A.It decreases
    • B.It stays the same
    • C.It increases as the square root of the load factor
    • D.It doubles for every G
    Show answer & explanation
    Answer: C. It increases as the square root of the load factor

    Stall speed rises proportional to √(load factor). At 2 Gs, stall speed is about √2 ≈ 1.41× the 1-G value.

  4. Question 4

    Ground effect is most noticeable when an airplane is:

    • A.At high altitude
    • B.Within approximately one wingspan of the surface
    • C.In a steep climb
    • D.Above pattern altitude
    Show answer & explanation
    Answer: B. Within approximately one wingspan of the surface

    Ground effect occurs within about one wingspan of the surface; reduced induced drag can allow a premature takeoff that then fails to sustain climb.

  5. Question 5

    Which of the following is NOT one of the four left-turning tendencies of a single-engine propeller airplane?

    • A.Torque
    • B.P-factor
    • C.Gyroscopic precession
    • D.Adverse yaw
    Show answer & explanation
    Answer: D. Adverse yaw

    The four left-turning tendencies are torque, P-factor, spiraling slipstream, and gyroscopic precession. Adverse yaw is a rolling-to-yaw coupling from differential aileron drag — a separate phenomenon.

48 more Aerodynamics & Systems questions are in the app, along with explanations and flashcards for every one.

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