Answer the following questions based on the chart on the next page. Identify your selected aircraft by case number (CC-AR6-1, CC-AR6-2, etc.). Note that there is more than one good answer for each question; identify one good candidate for each and why it is a good candidate to meet the requirement. 1. Which aircraft would likely perform best if the primary design goal was high speed, but less than Mach 0.5, and why is this so? 2. Which aircraft would likely perform best if the primary design goal was sustained flight at Mach 2.0, and why is this so? 3. Which aircraft would likely perform best if the primary design goal was maximum range at subsonic speed (less than Mach 0.5), and why is this so? 4. Which aircraft would likely perform best if the primary design goal was maximum endurance and speed was not important, and why is this so? 5. Which aircraft would likely have the lightest wing structural weight, and why is this so? Answers can be typed on a separate page or pages