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A vortex sheet is used in thin airfoil theory to represent

  • A.The shock wave at the leading edge
  • B.The camber line of the airfoil
  • C.The boundary layer on the surface
  • D.The wake far downstream of the wing

Answer: B

Correct answer: The camber line of the airfoil

Thin airfoil theory replaces the section by its mean camber line and distributes a sheet of vorticity along it, choosing the strength so that the camber line is a streamline and the Kutta condition is satisfied at the trailing edge. Because the model is inviscid it contains no boundary layer and no wake, which is precisely why it predicts lift accurately and drag not at all.

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