Question #7474

A plane is flying with a constant speed along a straight line at an angle of 60° with the
horizontal. The weight W of the plane is 90, 000 N and its engine provides a thrust T of
120, 000 N in the direction of flight. Two additional forces are exerted on the plane: the lift
force F perpendicular to the plane’s wings, and the force R due to air resistance opposite to
the direction of motion. Draw the free-body diagram showing all forces on the plane.
Determine F and R.

Expert's answer

A plane is flying with a constant speed along a straight line at an angle of 6060{}^{\circ} with the horizontal. The weight W of the plane is 90,000 N and its engine provides a thrust T of 120,000 N in the direction of flight. Two additional forces are exerted on the plane: the lift force F perpendicular to the plane's wings, and the force R due to air resistance opposite to the direction of motion. Draw the free-body diagram showing all forces on the plane. Determine F and R.



2-nd Newton's law in two projections:

1. F-axis


FWcos(60)=0F - W \cos (6 0) = 0F=Wcos(60)F = W \cos (6 0)F=90000Ncos(60)=45000NF = 9 0 0 0 0 N * \cos (6 0) = 4 5 0 0 0 N


2. R-axis


RT+Wcos(30)=0R - T + W \cos (3 0) = 0R=TWcos(30)R = T - W \cos (3 0)R=120000N90000Ncos(30)=42057.7NR = 1 2 0 0 0 0 N - 9 0 0 0 0 N * \cos (3 0) = 4 2 0 5 7. 7 N


Answer: F=45000NF = 45000N , R=42057.7NR = 42057.7N

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