The location of the center of pressure is often denoted as “xcp,” and its position along the chord of the airfoil or wing is a key parameter in aircraft design and stability analysis. Calculating the exact location of the center of pressure (xcp) can be complex, especially for varying angles of attack and different airfoil shapes.Â
- xcp: Location of the center of pressure along the chord
- cm,le: Moment coefficient about the leading edge
- c: Chord length of the airfoil
- cl: Lift coefficient of the airfoil