Drag Polar Calculation Post author:chandansingh Post published:October 7, 2020 Post category:Aerospace Calculator Post comments:0 Comments CD = CD0 + K.CL 2 Drag polar is the relationship between the lift on an aircraft and its drag, expressed in terms of the dependence of the drag coefficient on the lift coefficient. Wikipedia You Might Also Like Take Off Distance calculator June 4, 2021 Landing-gear weight equation May 11, 2021 Jet Velocity May 3, 2021 Leave a ReplyYou must be logged in to post a comment.