Skin Friction Coefficient given Flat Plate Area evaluator uses Skin Friction Coefficient = Flat Plate Area/(Form Factor Drag*Aircraft Wetted Area) to evaluate the Skin Friction Coefficient, The Skin Friction Coefficient given Flat Plate Area is a dimensionless quantity that characterizes the frictional drag generated by the airflow along the surfaces of an aircraft, this formula is defined as quantity that specifies the fraction of the local dynamic pressure and shear stress on the body. Skin Friction Coefficient is denoted by μf symbol.
How to evaluate Skin Friction Coefficient given Flat Plate Area using this online evaluator? To use this online evaluator for Skin Friction Coefficient given Flat Plate Area, enter Flat Plate Area (A), Form Factor Drag (Φf) & Aircraft Wetted Area (Swet) and hit the calculate button.