Aircraft Conventional Tail Assembly

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Questions and Answers

What is the purpose of a taileron in a modern air-superiority fighter?

  • To move the horizontal stabilizer surfaces for pitch control
  • To reduce the rolling power under all conditions
  • To provide additional control in roll (correct)
  • To increase the stiffness requirement of the vertical fin

Why is it important to design for minimum horizontal tail size in a T-tail arrangement?

  • To minimize the fin stiffness requirement (correct)
  • To increase the mass of the horizontal stabilizer
  • To reduce the rolling force under all conditions
  • To increase the stiffness requirement of the vertical fin

What effect does stabilizer dihedral have on the flutter speed in a T-tail design?

  • It reduces the required fin stiffness for flutter reduction (correct)
  • It increases the stiffness requirement of the vertical fin
  • It increases the mass of the horizontal stabilizer
  • It has no effect on flutter speed

What is the role of the jack arm in the variable incidence jackscrew connected to the horizontal stabilizer?

<p>To adjust the angle of incidence of the horizontal stabilizer (A)</p> Signup and view all the answers

What is the primary parameter for T-tail flutter?

<p>The vertical fin torsional stiffness (A)</p> Signup and view all the answers

In large transport planes, how is the angle of attack of the stabilizer adjusted?

<p>By means of an electrically driven or manually operated ball nut and jackscrew attached to the forward side of the center section (D)</p> Signup and view all the answers

What is the purpose of the rubber aerodynamic seal between the stabilizer sections and the aft fuselage?

<p>To prevent moisture from entering the gaps (A)</p> Signup and view all the answers

Which aircraft features an all-moving tailplane as shown in Fig. 10.1.3?

<p>Lockheed Jetstar (A)</p> Signup and view all the answers

What type of hinge joints are used for the stabilizer in large transport planes?

<p>Self-aligning bushing type hinge joints (C)</p> Signup and view all the answers

Which aircraft used the all-movable horizontal stabilizer (flying tail) as shown in Fig. 10.1.4?

<p>L-1011 transport (A)</p> Signup and view all the answers

What is the term for the load that occurs due to the stabilizer forced bending?

<p>Rib crushing (C)</p> Signup and view all the answers

Which term refers to the unsymmetrical spanwise load distribution on the fin?

<p>Dynamic overyaw (B)</p> Signup and view all the answers

What is the term for the load redistribution resulting from an actuator support?

<p>Concentrated load redistribution (A)</p> Signup and view all the answers

What is the term for the load caused by hail strike on the leading edge?

<p>Instantaneous elevator (D)</p> Signup and view all the answers

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