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Static Pitch Stability and Neutral Point
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Static Pitch Stability and Neutral Point

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Questions and Answers

What is the term for the percent distance from the neutral point to the center of gravity?

  • Pitching moment coefficient
  • Longitudinal stability margin
  • Static pitch stability
  • Static margin (correct)
  • What is the typical range of positive static margin for a transport aircraft?

  • 1-5%
  • 15-20%
  • 10-15%
  • 5-10% (correct)
  • What is the purpose of the computerized flight control system in an aircraft with relaxed static stability?

  • To deflect the elevator and provide artificial stability (correct)
  • To reduce trim drag
  • To provide artificial instability
  • To increase the pitching moment coefficient
  • What is the effect on the pitching moment derivative when the center of gravity is ahead of the neutral point?

    <p>It becomes negative</p> Signup and view all the answers

    What is the typical shape of the tailplane on a conventional aircraft?

    <p>Symmetrical aerofoil</p> Signup and view all the answers

    What is the effect of a negative static margin on an aircraft?

    <p>It becomes less stable</p> Signup and view all the answers

    What happens to the pitching moment when the downwash decreases the effective angle of attack?

    <p>It decreases</p> Signup and view all the answers

    What is the purpose of upward deflection of the elevators and downward deflection of the trim tab?

    <p>To increase the tailplane download</p> Signup and view all the answers

    What is the effect of high angles of attack on the CP?

    <p>It moves forward</p> Signup and view all the answers

    What is the main difference between the longitudinal and lateral-directional analyses?

    <p>The lateral-directional analysis resembles the longitudinal analysis</p> Signup and view all the answers

    What is the sign convention for the yawing moment derivative with respect to Beta?

    <p>A positive value indicates stability</p> Signup and view all the answers

    What is the primary function of the vertical tail in relation to the fuselage?

    <p>It counteracts the fuselage yawing moment</p> Signup and view all the answers

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