The formula for calculating wing twist can vary depending on the specific design and requirements of the aircraft. Generally, wing twist refers to the change in angle of incidence along the span of the wing.
Where:
- Twist angle is the change in angle of incidence along the span of the wing (in radians).
- Slope is the rate of change of angle of incidence per unit span (in radians per meter).
- Span is the wingspan of the wing (in meters).