(Solved): 2.(60pt) A two-dimensional supersonic wing has the profile, as shown in figure. (a) At zero angle o ...

2.(60pt) A two-dimensional supersonic wing has the profile, as shown in figure. (a) At zero angle of attack, determine the drag force on the wing per unit length of span at Mach number of \( 3.0 \). (b) Determine the lift force. Take the maximum thickness of the airfoil to be \( 0.2 \mathrm{~m} \).