Part 2: Now assume that the aircraft wing has a finite span of 10 meters Compute the thrust required for steady, level flight if the aircraft is to maintain a speed of 55 meters per second. Refer to the figure included below in order to calculate the span efficiency factor. Neglect viscous effects and assume incompressible flow in your calculations Part 3: Is the angle of attack required for steady, level flight for the aircraft in Part (b) less than greaterthan or equal to the angle of attackthatwas determinedin Part(a)? Explain why. 0.16 0.12 0.08 0.04 0.2 0.4 0.6 Taper ratio, c,/c, AR = 10 8 0.8 1.0