62. MA model airplane of mass 0.750 kg flies with a speed of 35.0 m/s in a horizontal circle at the end of a 60.0-m control wire as shown in Figure P7.62a. The forces exerted on the airplane are.shown in Figure P7.62b, the tension in the control wire, 0 = 20.0" inward from the vertical. Compute the tension in the wire, assuming the wire makes a constant angle ot 0320.0* with the horizontal. Circular path of airplane Wire Figure P7.62
62. MA model airplane of mass 0.750 kg flies with a speed of 35.0 m/s in a horizontal circle at the end of a 60.0-m control wire as shown in Figure P7.62a. The forces exerted on the airplane are.shown in Figure P7.62b, the tension in the control wire, 0 = 20.0" inward from the vertical. Compute the tension in the wire, assuming the wire makes a constant angle ot 0320.0* with the horizontal. Circular path of airplane Wire Figure P7.62
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A model airplane of mass 0.750 kg flies with a speed of 35 m/s in a horizontal circle at the end of a 60.0 m control wire as shown (See P7.62a) The forces exerted on the airplane are shown (See P7.62b), the tension in the control wire, angle = 20.0 degrees inward from the vertical. Compute the tension in the wire, assuming the wire makes a constant angle of 20.0 degrees.

Transcribed Image Text:62. MA model airplane of mass 0.750 kg flies with
a speed of 35.0 m/s in a horizontal circle at the end
of a 60.0-m control wire as shown in Figure P7.62a.
The forces exerted on the airplane are.shown in
Figure P7.62b, the tension in the control wire, 0 =
20.0" inward from the vertical. Compute the tension in
the wire, assuming the wire makes a constant angle ot
0320.0* with the horizontal.
Circular path
of airplane
Wire
Figure P7.62
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