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A supercritical aerofoil differs from a conventional section principally in having

  • A.A sharp leading edge
  • B.No camber at all
  • C.A flattened upper surface and pronounced aft camber
  • D.A much greater thickness ratio throughout

Answer: C

Flattening the crest keeps the local supersonic region at a modest Mach number over a long run, so the shock closing it is weak and both wave drag and shock-induced separation are reduced. The aft camber restores the lift that flattening the crest gave away, at the cost of a more nose-down pitching moment.

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