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Increasing the wing aspect ratio raises the lift curve slope because

  • A.The Reynolds number falls
  • B.The aerofoil section becomes thinner
  • C.Less of the section slope is lost to induced downwash
  • D.The wing area increases

Answer: C

A higher aspect ratio means weaker tip effects, so less of the section slope is eaten by induced downwash, and the finite-wing slope moves closer to the two-dimensional \( 2\pi \). The relation \( C_{L_\alpha} = a_0/(1 + a_0/\pi A) \) shows it directly. Aspect ratio is a shape parameter and does not by itself change area, which is held fixed in the comparison. Reynolds number depends on chord and speed, and the section thickness is unchanged.

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