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Excluding constants, the coefficient of induced drag (CDI) is the ratio of:
  • A
    CL² and AR (aspect ratio).
  • B
    CL and b (wingspan).
  • C

    CL and AR (aspect ratio).

  • D
    CL and CD.

The induced drag can be defined by:

CDI = CL2 / π * AR

Where,
CDI – Induced Drag Coefficient
CL2 – Lift Coefficient squared
AR – Aspect Ratio

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