Answer
option A)
21,300 N
Step-by-step explanation
Given that,
mass of plan = 5320kg
altitude at which plan is flying = 2910m
drag force = 530N
Number of forces acting on airplane
1)
Downward Force
weight = mg
= 5320(9.81)
= 52189.2 N
2)
Lifting Force
3)
Force that push the airplane forward, thrust
4)
Force that opposes thrust, drag
Since plane is horizontal it means weight = lifting force, this balance out.
So, in order to calculate thrust which engines exert in order for the airplane to accelerate at 4.10 m/s²
Fnet=ma or ΣF = ma,
where Fnet (or ∑F) is the net external force,
Fnet = Thrust - frictionalForce(drag)
ma = T - f
5320(4.10) = T - 530
21812 = T - 530
21812 - 530 = T
T = 21282 N
T ≈ 21,300 N