Drag polar calculator – K.prakashbalan Post author:prakashbalan Post published:October 16, 2020 Post category:Aerodynamics Calculator / Aerospace Calculator / Aircraft Design / Airplane Performance Calculator / Flight Mechanics Calculator Cd=Cd0+K Cl^2 Drag polar is the relationship between lift on an aircraft and its drag, expressed in terms of dependence of drag coefficient on lift coefficient. It may be described by an equation as above. You Might Also Like Taper Ratio Calculator by Mohit Kudal February 7, 2021 pitch rate calculator April 10, 2021 Kinematics Coefficient of Viscosity Calculator March 17, 2021