Follow the DR$-1$ example given in Raymer Ch$.24($Conceptual Design Examples$)$ to carry out the aerodynamics calculations at cruise speed $($ Vcr $)$ and Sea$\_$Level $(h=0ft,)$ for your Sports$/$Trainer aircraft

i$)$ Calculate the Maximum lift coefficient and the Lift curve slope.

ii$)$ Calculate the Total parasite drag using the Component Buildup Method and the "Drag$-$due$-$to$-$lift factor" $($K$).$ Then, by changing the Vcr in the $(0-$ Vmax$)$ kt interval, prepare a $)$ table $($similar to one given in S: $893,$ Raymer, $6$th ed$),$ plot your Drag Polar $C_L-C_D$ curve$).$