(b) Code in MATLAB. An Airbus A320 is flying at Mach 0.5. It's Pitot tubes, shown in Figure 2, measure the total, or stagnation, pressure (pressure when the air hits and is stopped by the tube) as well as the static free-stream pressure The ratio of total to static pressure is determined to be: Po/p 1.186. The following equation relates this change in pressure to the inlet Mach number, M, and , the heat capacity ratio PITOT TUBE Pitot tube e 2: Pito-Static Tubes: They measure the ratio of total pressure to static pressure to mine the aircraft airspeed Based on the given pressure ratio and Mach number, determine the value of that satisfies this equation to 5 significant figures of accuracy. State what method you used, how many iterations it took and give your final solution estimate. Hint: Don't try to solve analytically for y. It might be helpful to plot the function f() over a range of values to help you pick a good initial first guess. Choose from any of the iterative methods learned in class to solve