Wing camber Calculator

The wing camber formula depends on the specific airfoil shape being used. One common formula for camber line calculation is the NACA 4-digit series formula, which determines the camber line based on a series of parameters.

Where:

  • is the camber line’s vertical position,
  • is the maximum camber as a fraction of the chord length,
  • p is the location of the maximum camber as a fraction of the chord length, and
  • is the distance along the chord from the leading edge.

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