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A wing carrying a distributed aerodynamic torque along its span will have a rate of twist that

  • A.Is zero everywhere
  • B.Is largest at the tip
  • C.Varies along the span
  • D.Is constant along the span

Answer: C

The torque accumulates from tip to root, so it is largest at the root, and with the box also tapering the rate of twist varies along the span. The total tip twist is found by integrating the local rate along the length.

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