Griffin Z. answered 07/20/26
UC Berkeley MechE PhD tutoring Advanced Physics for Engineers
This problem utilizes the principles of vertical force equilibrium and centripetal force in uniform circular motion.
We first take note of the given quantities:
Length of wire l = 18.5 m
Angle with horizontal θ = 27.0°
Tension in wire T = 140 N
Mass of airplane m = 3.26 kg
Acceleration due to gravity g = 9.8 m/s²
We then identify the unknown quantities:
(a) Lift force acting on the plane L = ?
(b) Speed of the plane v = ?
For part (a), we balance the forces in the vertical direction where acceleration is zero:
L cosθ - T sinθ - mg = 0
We rearrange to isolate and solve for L:
L = (T sinθ + mg) / cosθ
L = (140 N * sin(27.0°) + 3.26 kg * 9.8 m/s²) / cos(27.0°)
L = 175.9 N
For part (b), we apply Newton's second law in the horizontal direction. The radius of the horizontal circular motion is:
r = l cosθ
The horizontal components of the lift and tension forces provide the net centripetal force:
m * a = m(v² / r) = L sinθ + T cosθ
Substituting r = l cosθ into the equation:
m(v² / (l cosθ)) = L sinθ + T cosθ
We rearrange to isolate and solve for v:
v = sqrt( l cosθ * (L sinθ + T cosθ) / m )
v = sqrt( 18.5 m * cos(27.0°) * (175.9 N * sin(27.0°) + 140 N * cos(27.0°)) / 3.26 kg )
v = 32.16 m/s