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A section has a lift curve slope of \(0.11\) per degree and a zero-lift angle of \(-2^\circ\). Its lift coefficient at \(6^\circ\) is about

  • A.0.88
  • B.0.66
  • C.0.44
  • D.1.10

Answer: A

Correct answer: 0.88

The lift coefficient is proportional to the angle measured from the zero-lift angle, not from the chord line: \[ c_l = a_0(\alpha - \alpha_{L=0}) = 0.11\,(6 - (-2)) = 0.11 \times 8 = 0.88. \] Measuring from zero incidence instead gives 0.66, which is offered as a distractor. For a cambered section the zero-lift angle is negative, so the effective angle is always the larger of the two.

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