AviationTire Principles Of Flight - Aeroplane Subsonic Aerodynamics Means to decrease the CL - CD ratio, increasing drag Q 1 / 5

The maximum lift-to-drag ratio for an aircraft 13,6. Calculate the minimum glide angle and the maximum range measured along the ground covered by the airplane in a power-off glide that starts at an altitude of 10.000ft.

Minimum glide angle = 4.2 degrees, maximum range = 25.6 miles.
Minimum glide angle = 3.2 degrees, maximum range = 15.6 miles.
Minimum glide angle = 5.2 degrees, maximum range = 35.6 miles.
Minimum glide angle = 2.2 degrees, maximum range = 25.6 miles.