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For a wing of finite span in inviscid, incompressible flow, d'Alembert's paradox

  • A.Does not apply, because the trailing vortex system leaves a wake
  • B.Applies exactly, so the drag is zero
  • C.Applies only above the stalling angle
  • D.Predicts infinite drag at all angles of attack

Answer: A

The paradox states that a closed body in steady inviscid flow experiences no drag, but its derivation assumes no wake and no vorticity left behind. A lifting wing of finite span violates that assumption: it trails vorticity indefinitely downstream. Induced drag is therefore a genuine inviscid drag and no contradiction arises.

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