Drag coefficient in turning flight calculator

In flight mechanics, the “drag coefficient” (CD) in turning flight refers to the dimensionless parameter that quantifies the drag force acting on an aircraft during a turn. It is a crucial factor in understanding the aerodynamic performance of the aircraft while maneuvering.
Ta / (0.5 * ρ * V^2 * S)
  • Ta: Thrust force acting on the aircraft. It is the force generated by the aircraft’s engines or propulsion system to overcome drag and provide forward thrust.
  • ρ: Air density. It is the mass of air per unit volume and depends on altitude and atmospheric conditions.
  • V: Airspeed or true airspeed of the aircraft.
  • S: Reference area of the aircraft. In the context of the Thrust-to-Drag Ratio, it is usually the wing area.

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