A model airplane of mass m = the end of an L = 60.0-m control wire as shown in the figure below. The forces acting on the 0.570 kg flies with a speed of v = 28.0 m/s in a horizontal circle at airplane are shown in the free body diagram below. Suppose 0 = 23.0°. Find the tension in the control wire. Assume the lift force Fiift is perpendicular to the wings. Figre L rotation axis Figure a (side view control wire wings of ai rplane horizontal Grcular pat h of air plane

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Chapter6: Applications Of Newton's Laws
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A model airplane of mass m = 0.570 kg flies with a speed of v = 28.0 m/s in a horizontal circle at
the end of an L = 60.0-m control wire as shown in the figure below. The forces acting on the
%3D
airplane are shown in the free body diagram below. Suppose 0 = 23.0°. Find the tension in the
%3D
control wire. Assume the lift force Fift is perpendicular to the wings.
Figre I
rotation
axis
Figure a (side view
of airplene)
Fages
control
wire
..
wings of
airplane
horizontal
Gtcular pat h
of airplane
Transcribed Image Text:A model airplane of mass m = 0.570 kg flies with a speed of v = 28.0 m/s in a horizontal circle at the end of an L = 60.0-m control wire as shown in the figure below. The forces acting on the %3D airplane are shown in the free body diagram below. Suppose 0 = 23.0°. Find the tension in the %3D control wire. Assume the lift force Fift is perpendicular to the wings. Figre I rotation axis Figure a (side view of airplene) Fages control wire .. wings of airplane horizontal Gtcular pat h of airplane
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