Consider the aircraft in Problem 12 is on a runway at 3000 ft altitude. The aircraft side area is 16 m 2 , and the height of the aircraft centroid of side area from the ground is 1.2 m. A cross-wind...

Consider the aircraft in Problem 12 is on a runway at 3000 ft altitude. The aircraft side area is 16 m², and the height of the aircraft centroid of side area from the ground is 1.2 m. A cross-wind with a speed of 30 knot is blowing. Assume the aircraft side drag coefficient is 0.7. Determine the minimum wheel track to prevent an overturn due to this cross-wind. The lowest possible mass is 2000 kg when there is no passenger onboard and zero fuel.