Drag coefficient Calculator

The drag coefficient (Cdw) represents the amount of aerodynamic drag generated by the wing relative to the dynamic pressure of the air and the wing area.

Where:

  •  Dw is   Drag wing is the drag force generated by the wing.
  • ρ (rho) is the air density.
  • V is the airspeed of the aircraft.
  • S_wing is the wing area.

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