✔ 最佳答案
(b) Because the lifting force is always acting perpendicular to the wings, when the aircraft is banked, the lifting force becomes tilted at some angle with the vertical. This provides a horizontal force component, giving the necessary centripetal force for the aircraft to turn around.
(d) Let F be the total lifting force, and a be the angle at which the aircraft is banked.
Hence, we have,
Horizontally, F.sin(a) = mv^2/R
where m is the mass of the aircraft
v is the speed of the aircraft
R is the radius of the turn
Vertically, F.cos(a) = mg where g is the acceleration due to gravity
Dividing, sin(a)/cos(a) = v^2/Rg
i.e. tan(a) = (500/3.6)^2/4000 x 10 (take g = 10 m/s^2)
a = 25.75 degrees
Therefore, F = mg/cos(25.75) N = 27,760 N