3. (4 points) Use Newtonian theory to calculate the drag coefficient over the capsule-like section (ABCB'A') shown below for hypersonic flow. Use capule verti- cal height as reference length. Do not assume small angles. Use polar coordinates to obtain analytical solution, and use x-y coordinates and Matlab to produce an integrated solution. (0.0 , 3.0) ABC = VR - x2 C M > > 5(-2.0, 2.12) B R = 3m B' (2.0, 2.12) 45 14. K = 3m (0.0 , 0.0) (-1.0,- 2.0) A A' (1.0, -2.0)