Aviation Dictionary
ضریب مرکز فشار بال، نسبت فاصله مرکز فشار تا لبه حمله به طول وتر (chord) بال
The distance between the leading edge of an airfoil and the location of the center of pressure expressed as a ratio of this distance to the length of the airfoil chord line. If the center of pressure coefficient, which is expressed as cp on a set of airfoil characteristic curves, is 0.3, the center of pressure is located 30% of the chord line length behind the leading edge of the airfoil.