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A model airplane of mass 0.820 kg flies with a speed of 35.0 m/s in a horizontal circle at the end of a 54.0-m-long control wire as shown in Figure (a). The forces exerted on the airplane are shown in Figure (b): the tension in the control wire, the gravitational force, and aerodynamic lift that acts at 0 = 20.0° inward from the vertical. Compute the radius, lift, and tension in the wire, assuming it makes a constant angle of 8=20.0 with the horizontal, Use g-9.8 m/s². radius 50.7 lift 19.81 Your response differs from the correct answer by more than 10%. Double check your calculations. N tension 15.87 Circular path of airplane Wire

A model airplane of mass 0.820 kg flies with a speed of 35.0 m/s in a horizontal circle at the end of a 54.0-m-long control wire as shown in Figure (a). The forces exerted on the airplane are shown in Figure (b): the tension in the control wire, the gravitational force, and aerodynamic lift that acts at 0 = 20.0° inward from the vertical. Compute the radius, lift, and tension in the wire, assuming it makes a constant angle of 8=20.0 with the horizontal, Use g-9.8 m/s². radius 50.7 lift 19.81 Your response differs from the correct answer by more than 10%. Double check your calculations. N tension 15.87 Circular path of airplane Wire

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A model airplane of mass 0.820 kg flies with a speed of 35.0 m/s in a horizontal circle at the end of a 54.0-m-long control wire as shown in Figure (a). The forces exerted on the airplane are shown in Figure (b): the tension in the control wire, the gravitational force, and aerodynamic lift that acts at 0= 20.0° inward from the vertical. Compute the radius, lift, and tension in the wire, assuming it makes a constant angle of 0-20.0° with the horizontal, Use g-9.8 m/s². radius 50.7 lift 19,81 x Your response differs from the correct answer by more than 10%. Double check your calculations. N tension 15.87 Circular path of airplane Wire
Transcribed Image Text:A model airplane of mass 0.820 kg flies with a speed of 35.0 m/s in a horizontal circle at the end of a 54.0-m-long control wire as shown in Figure (a). The forces exerted on the airplane are shown in Figure (b): the tension in the control wire, the gravitational force, and aerodynamic lift that acts at 0= 20.0° inward from the vertical. Compute the radius, lift, and tension in the wire, assuming it makes a constant angle of 0-20.0° with the horizontal, Use g-9.8 m/s². radius 50.7 lift 19,81 x Your response differs from the correct answer by more than 10%. Double check your calculations. N tension 15.87 Circular path of airplane Wire
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